Thursday Plenary Session 9:00

Humans to Mars within a Decade

Robert Zubrin

Pioneer Astronautics

445 Union Blvd. #125

Lakewood, CO 80228

We currently have the technology required to establish a permanent human presence on Mars within 10 years at a cost of roughly 15% of the existing NASA budget. The key is to adopt a "live-off the land" philosophy, making rocket propellants and other necessary mission consumables on the surface of Mars. This paper will discuss how this can be done, and the significance of such a step in the context of the development of humanity from a single planet to a multi-planet species.

Thursday Plenary Session 10:00

Biogenic Activity in Martian Meteorite ALH84001

Everett K. Gibson, Jr

David S. McKay

NASA Johnson Space Center

Houston, TX

Kathie Thomas-Keprta

Lockheed Martin

The Martian meteorite ALH84001 has been shown to contain evidence of possible past biogenic activity inside small carbonate aggregates or globules within the meteorite. Four lines of evidence presented by McKay et al. (1) included: (a) iron oxides and sulfides having textures similar to terrestrial biominerals, (b) carbonates formed at temperatures capable of supporting biogenic activity, (c) indigenous organic compounds associated with the carbonate globules, and (d) morphologies of segmented, spherical and elongated features similar to terrestrial micro fossils. None of these observations is in itself conclusive for the existence of past life. Although there are alternative explanations for each of these phenomena taken individually, when they are considered collectively, particularly in view of their close spatial association, it was concluded that they were evidence for primitive life on Mars. Since our report (1) additional observations have been made which support our hypothesis: (i.) carbon isotropic compositions (-18 to –20 %), (ii) biofilm-like textures, (iii) chains of magnetite grains similar to those produced by magnetotactic bacteria, and (iv) oxygen isotropic compositions with in individual globules that show low temperature processes (2). Alternative hypotheses for the origins of the carbonate globules have been directed toward the formation temperatures, magnetite morphologies and structures within the carbonates, the sizes of nanostructures within carbonate rims, and potential terrestrial organic contaminants (i.e. PAHs). The evidence, both pro and con, will be critically evaluated in light of recent research that has been conducted since the initial hypothesis of past biogenic activity in the Martian meteorite ALH84001.

  1. D.S. McKay et al., Science 273, 924-930 (1996)
  2. Refs. Within Lunar and Planetary Science- 28th and 29th abstracts (1997 and 1998)

Thursday Plenary Session 11:00

NASA's Robotic Mars Exploration Program

Rob Manning

Jet Propulsion Lab

Pasadena, CA

NASA’s recent accomplishments and current plans for the exploration of Mars using robotic technology will be presented.

Thursday Plenary Session 11:30

An Arctic Mars Base

Pascal Lee

NASA Ames Research Center

Moffett Field, CA

It is proposed that the Mars Society build a simulated Mars exploration base in the Canadian Arctic

12:00 break

Thursday Plenary Session 1:00

Exploring Mars with Balloons / France and the US Together to Mars

Jacques Blamont

CNES France

This talk will consist of two components. In the first part, the superb potential of balloons for carrying out robotic exploration of Mars from aerial platforms will be discussed. In the second part, the author will discuss plans currently being negotiated at the ministerial level for a joint US-French program for Mars exploration.

Track 1A 2:00

Thinking About Martian Economics

Ed Hudgins

The Cato Institute

Washington DC

Why, four decades after men first ventured into space are there no regularly scheduled commercial flights into orbit? Some 35 years after the Wright brothers 1903 flight the commercially viable DC-3 was flying. But today the cost of placing payloads into orbit on the Shuttle is perhaps a magnitude more than on Apollo. By contrast, in the past twenty years the cost of airline tickets per mile dropped by 30 percent, with twice as many people now flying, and the cost of shipping oil dropped 80 percent. For too long space enthusiasts have ignored economics at the peril of their passion.

The most economically and politically viable approach to a Mars mission, based on market principles, is the Mars Prize approach, supported by House Speaker Gingrich. A $20 billion prize, with an actual mission cost of only $5 billion, indeed creates an incentive for the private sector to find the best way to the Red Planet. But these funds still have proven difficult to secure. Mars enthusiasts might support a radical approach: as part of a strategy to return civilian space efforts to the private sector, the planned space station could be scrapped. Some of the savings would go the Mars Prize and would help promote that civilian sector.

But at $5 billion, a consortium of enterprises and educational institutions could fund a Mars mission. Yet without taxpayers funds, what would be the incentive to go? The prospect of property rights and owning Martian assets would be a strong incentive. Also a consortium might earn money and develop technology for a Mars mission by taking on other tasks for profit. For example, a Disney Company might put up several hundred million dollars to put camera-equipped rovers on the Moon to provide holodeck-type virtual reality entertainment on Earth. The road to Mars does not have to go through government territory.

Track 1A 2:30

Privately Financing a Mars Expedition : The Olympic Model

Stewart Money

273 Willow Lane #8-B

McDonough, GA 30254

Csmoney@bellsouth.net

In order to be sustainable, any program of manned Mars exploration will require the lowest possible transportation and infrastructure costs. As evidenced by the Space Shuttle and International Space Station programs, such a requirement is simply incompatible with publicly funded space endeavors.

Consequently, the first expedition to Mars must be privately financed and managed. Accomplishing this will require a new organization, one specifically designed to fill the gap between what government is unable to accomplish efficiently, and what purely private industry is unable to do profitably.

A precedent can be found in the 1996 Centennial Olympic Games in Atlanta, the first privately financed Olympic Games. Costing $1.7 billion, or approximately 25% of a privately managed Mars mission as described in The Case for Mars, the 1996 games actually made money while leaving behind as permanent infrastructure $550 million in athletic facilities and parks.

These results were possible because the Olympics were managed through a unique arrangement in which a privately organized, publicly endorsed organization, the Atlanta Committee for the Olympic Games, was vested with the authority to negotiate advertising and sponsorship agreements with the entire spectrum of potential sponsors, from major corporations such as IBM, Coca-Cola, Delta, NationsBank and Home Depot, down to individual street vendors.

While the Summer Olympics are certainly a major media event, they pale beside what stands to be the biggest story of our time, the first human voyage to Mars. By this standard, the global marketing opportunity which made the Olympics attractive to corporate sponsors are even more pronounced. Quite simply, Mars represents a marketing potential so vast as to challenge the imagination.

This paper examines a number issues involved with privately funding an initial series of manned Mars expeditions following the Atlanta Olympic Model.

Track 1A 3:00

Possible Design of First Privately-Funded Mars Surface Exploration Probe:

Ruthless Minimalism Approach

Tomas Svitek

Stellar Innovations, Inc.

1436 Clover Creek Dr.

Longmont CO 80503

What is the absolutely lowest possible cost for a small unmanned Mars probe that lands on the surface and performs interesting exploration from the public point of view? We have been asking this question for many years. We are after the true lowest-cost mission, not assuming the free labor or donated hardware.

Therefore, the only free variable is to reduce the mission complexity, simplify or even eliminate most of the hardware and software that would have been carried on a ordinary (government-funded) mission. We have seen many useful low-Earth-orbit missions that were developed for around a million dollars. The lowest-cost deep-space missions were about 50-100 more expensive. The conventional wisdom says that this is due to the more demanding requirements of a deep-space mission.

Our paper will address this point of view and attempt to demystify the deep-space spacecraft design. Clearly, there are many difficult and challenging missions in the solar system. But we want to show that a simple modest Mars mission can be within a reach of the community that successfully launched dozens low-cost Earth-orbiting spacecraft.

We will present the point design for such a mission in our paper. It is not going to satisfy specific scientific objectives but rather offer an interesting exploration challenge to the interested public.

Track 1A 3:30

Paying for the Greatest Adventure in Human History

Chris Cowlin

8607 Gosling Way

Powell, Ohio 43065

Subject:

My paper offers a proven funding solution for the entire Mars mission. The formation, governance and operation of a self-perpetuating corporation devoted solely to the mission will be described in detailed but understandable terms.

Point of View:

Success depends on three factors:

  1. Raising funds adequate for a successful and profitable mission while avoiding all forms of government funding.
  2. Creating a reliable cash flow from each stage of the mission’s development
  3. Making solid provisions for mission continuation after the first touch down.

Operational Structure:

Bureaucracies can’t execute the mission with any reasonable hope of success. A credible and authoritative corporate entity exercising executive control over all aspects of the mission is essential. Scientific quests, entrepreneurial development, high-risk technology and innovative financial structures are best left to the few interested parties willing to make the commitments and sacrifices necessary for success. The solution: The Martian Expeditionary Foundation (MEF).

The MEF solves the critical issues of control, ownership, and continuation. The MEF is a on going self-managed trust sponsoring mission activities until conventional corporate mechanisms are able to assume day-to-day responsibilities. The MEF raises capital, makes binding commitments, obtains copyrights and controls licensing revenue. At opportune moments, the MEF will bundle assets (mission materials, copyrights, etc.) with liabilities (debt, payroll, operating cost, etc.) and offer fully formed space-based corporations (stock) to interested investors. In turn, the MEF employs the cash received for further development.

Sources of Revenue:

The MEF has at least five revenue sources, all based on the sales of:

  1. Mission Data
  2. Memorialization
  3. PR, endorsement and logo opportunities
  4. Martian material
  5. Copyrights

Summary:

The paper provides a blueprint for financial success. Mankind’s greatest adventure needs a solid business mechanism that insures success. Bold leadership combined with conservative solid execution will get us to the red planet

Track 1A 4:00

Funding the First Human Expedition t Mars

George Osorio
osorio#d#george@ssdgwy.mdc.com

A proposition is made that, given past experience with government space exploration programs, the first human expedition to the Red Planet can be funded entirely from private or commercial sources without depending primarily on financial support from the US government.  The steps needed to obtain such funding are described and suggested examples are considered, including plausible Mars exploration scenarios.  Based on the information presented, a case is made for proceeding directly with the development of a human expedition to Mars, funded entirely from private sources, while leaving the robotic missions to NASA/JPL and other government entities, including internationals.  

Track 1A 4:30

Paying for the Trip

Jim Beyer

beyer@pilot-ind.com

Another financing plan to pay for a ‘Mars Direct’ manned expedition to Mars is presented. Although at least three other plans for funding exist; all of these alternatives have flaws which limit their practical implementation. By using the positive points which each of these plans have, a new plan is developed which can succeed and (perhaps more importantly) can be implemented immediately.

A key point to this plan is to exploit a resource that is immediately available and saleable on the first Mars expedition. This substantial resource could pay for a majority of an expedition by itself, but has not been mentioned, even in passing, in the book, "The Case for Mars". Other resources are brought into play that can cover the remainder of the costs. It is assumed that a private concern could develop an expedition in the range of $15 billion. A lower cost expedition could be financed even more easily; a higher cost would be increasingly less practical to fund. Central to any funding effort is the improved estimation of the expedition cost. Current cost estimates range broadly from $4 billion to $50 billion.

Although there are no real templates for this sort of fund-raising effort; some analogues exist. The University of Michigan embarked on a $1 billion fund-raising effort some years ago: they raised $1.2 billion. Harvard University, with a smaller (but perhaps wealthier) alumni pool, has launched an even more ambitious fund-raising effort. The Mars effort suffers from a lack of credibility compared with centuries old educational institutions, but surpasses these institutions in its broad appeal; potentially to every member of humanity.

 

Track 1A 5:00

The Business of Commercializing Space

David M. Livingston

 

This paper will investigate and report on some of the important business issues facing the commercialization of space, including private sector projects to the moon and Mars. One important issue concerns the potential conflicts of interest and competition among the various government agencies exercising regulatory control over certain aspects of commercial space development. These potential jurisdictional conflicts involve the FAA, NASA, The Department of Commerce and the FCC. The advantages and disadvantages of the roles of these regulatory agencies from both a business and space consumer’s perspective will be discussed.

Financing commercial space projects will also be addressed, especially the use of venture capital as this is a frequently mentioned private sector tool for funding various commercial space projects and programs. With financing in mind, a look at various new space industries will be undertaken, as these industries have both applications and implications for private sector space commercialization and for investing and operating private sector missions to the moon and Mars, and for the popular emerging space tourism industry.

The final component of this paper discusses both the quality and the character of the business that we take off this planet to explore and develop space in general, and use in establishing bases and settlements on the moon and Mars. Perhaps not all our business practices, philosophies, procedures and attitudes are qualities we want to export off the earth. How shall we live, work and play in space, on the moon and on Mars is a question that needs to be considered. We will be the first society to begin the process of living, working and playing in space, and establishing settlements and colonies off this planet. With this honor and privilege also comes the responsibility to seed our future generations of space inhabitants, businessmen and women and leaders with a foundation, but what will that foundation look like? The consequences of what and how we carry out our development, commercialization, and colonization will remain with us for a very long time, both on earth and in space. This paper will address this important issue, an issue that can have an enormous impact on our space development plans extending not just to Mars but beyond Mars as well.

 

Track 2A 2:00

The Mars Pathfinder Mission and Science Results

A. F. C. Haldemann, M. P. Golombek, W. M. Folkner,T. J. Parker, J. T. SchofieldJet Propulsion Laboratory

T. EconomouUniversity of Chicago, Enrico Fermi Institute

H. J. Moore

U.S. Geological Survey

R. RiederMax Planck Institute for Chemistry, Germany

P. H. SmithLunar and Planetary Laboratory, University of Arizona,

Mars Pathfinder successfully landed on the surface of Mars on July 4, 1997, deployed and navigated a small rover, and collected data from 3 science instruments and 10 technology experiments. The mission operated for 3 months and returned 2.3 Gbits of new data, including over 16,500 lander and 550 rover images, 16 chemical analyses of rocks and soil, and 8.5 million individual temperature, pressure and wind measurements. The mission captured the imagination of the public, garnered front-page headlines during the first week, and became the largest internet event in history. From the science standpoint, the top results include: 1. Chemical analyses indicate some rocks may be high in silica implying differentiated parent materials. 2. Rounded pebbles and cobbles and a possible conglomerate observed with rover and lander images suggest fluvial processes that imply liquid water in equilibrium with the atmosphere and thus a warmer and wetter past. 3. The moment of inertia discerned from two-way ranging measurements to the lander, indicates a central metallic core of 1300-2000 km in radius. 4. Composite airborne dust particles collected by the magnet experiment appear magnetized by freeze dried magnetite stain or cement that may have been leached from crustal materials by an active hydrologic cycle. 5. Remote sensing data at a scale of generally greater than ~1 km and an Earth analog correctly predicted a rocky plain safe for landing and roving with a variety of rocks deposited by catastrophic floods that are relatively dust free. 6. Lander imaging found water ice clouds in the early morning atmosphere, while the meteorological package observed significant temperature time- and height-variability near the ground, as well as discovering dust-devil phenomena which have since been confirmed lander images.

Track 2A 2:30

The Martian Dust Cycle

Peter H. Smith
Lunar and Planetary Lab
University of Arizona
Tucson, Arizona

Mars Pathfinder’s IMP camera returned several thousand images of the Sun and sky that have been analyzed to understand the opacity over time and the physical and optical properties of the Martian dust.  In addition, magnets and targets on the lander were positioned to gather dust as it settled out of the atmosphere.  Dust devils have also been discovered in horizon images from the gallery pan.  Taken together the Martian dust cycle can begin to be understood from its source in the dust devils to the reservoir carried in the lower atmosphere to the sedimentation of the fine dust onto the surface.  In addition, the evidence for transport of the surface dust is seen in the Pathfinder images.  Ventifacts on the local rocks, duneforms and wind tails are evident around the site.  Windsocks measured the local winds and the ASI/MET instrument also observed wind directions and vortical winds passing the site.  Little change was observed between the Viking and Pathfinder eras suggesting that these are the conditions that any future mission, manned or robotic, will have to endure.  The current understanding of the dust cycle will be presented.

 

Track 2A 3:00

Mars Volatiles and Climate Surveyor (MVACS) Integrated Payload for the

Mars Polar Lander Mission

D. A. Paige (UCLA), W. V. Boynton (UA), D. Crisp (JPL), E. DeJong

(JPL), A. M. Harri (FMI), C. J. Hansen (JPL), H. U. Keller (MPAe), L.

A. Leshin (UCLA), P. H. Smith (UA) and R. W. Zurek (JPL)

The Mars Volatiles and Climate Surveyor (MVACS) integrated payload for the Mars Polar Lander will be launched in January, 1999, and land on Mars' south polar layered deposits in December, 1999. Over the course of its 90-day nominal mission during the Martian southern spring and

summer seasons, it will make in-situ measurements which will provide new insights into the behavior and distribution of Martian volatiles. MVACS consists of four major instrument systems: A Surface Stereo Imager (SSI) which will acquire multi-spectral stereo images of the surface and atmosphere; a 2-meter Robotic Arm (RA) which will dig a 0.5 meter deep trench and acquire surface and subsurface samples which will be imaged by a focusable Robotic Arm Camera (RAC) which will take close-up images of surface and subsurface samples at a spatial resolution of 21 microns; a Meteorology Package (MET) which will make the first measurements of surface pressure, temperature and winds in Mars' southern hemisphere and employ a Tunable Diode Laser (TDL) spectrometer to measure the water vapor concentration and isotopic composition of carbon dioxide in the Martian atmosphere; and a Thermal and Evolved Gas Analyzer (TEGA) which will use differential scanning calorimetry and TDL evolved gas analysis to determine the concentrations of ices, adsorbed volatiles and volatile-bearing minerals in surface and sub-surface soil samples. The unique in-situ measurements made by MVACS at its high-latitude landing site will

define a number of important aspects of the physical, isotopic and chemical nature of the Martian near-surface and sub-surface environment which will be valuable for better understanding of Mars

meteorites and returned samples, as well as the search for Martian resources which could be utilized by humans.

Track 2A 3:30

Mars Environmental Compatibility Assessment (MECA) - Identifying the Hazards of the Martian Soil

T. P. Meloy1, M. H. Hecht2, M. S. Anderson2, M. A. Frant3, S. Fuerstenau2, H. U. Keller4, W. Markiewicz4, J. Marshall5 W. T. Pike2, C. Quate6, J. D. Rademacher2, M. W. Shellman2, W. W. Schubert2, and P. Smith7

1. W. Virginia University, 338 COMER, P.O. Box 6070, Morgantown, WV 26506 USA

2. Jet Propulsion Laboratory, 4800 Oak Grove Dr., Pasadena, CA 91109 USA

3. Orion Research, Inc., 131 Westchester Rd., Newton, MA USA

4. Max Planck Institute fur Aeronomie, P.O. Box 20, D-37189 Katlenburg-Lindau, Germany

5. SETI Institute NASA ARC, M/S 239-12, Moffett Field, CA 94035-1000 USA

6. Stanford University, Ginzton Laboratory, Stanford, CA 94305-9045 USA

7. University of Arizona, Lunar and Planetary Laboratory, Tucson AZ 85721 USA

Sometime in the next decade, NASA will decide whether to send a human expedition to explore the planet Mars. The Mars Environmental Compatibility Assessment (MECA) has been selected by NASA to evaluate the Martian environment for soil and dust hazards to human exploration. The integrated MECA payload contains three elements: a wet-chemistry laboratory, a microscopy station, and enhancements to a lander robot-arm system incorporating arrays of material patches and an electrometer to identify triboelectric charging during soil excavation.

The wet-chemistry laboratory will evaluate samples of Martian soil in water to determine the total dissolved solids, redox potential, pH, and quantify the concentration of many soluble ions using ion-selective electrodes. These electrodes can detect potentially dangerous heavy metal ions, emitted pathogenic gases, and the soil's corrosive potential.

MECA's microscopy station combines optical and atomic-force microscopy with a robot-arm camera to provide imaging over nine orders of magnitude, from meters to nanometers. Through a careful selection of sample receptacles and an abrasion tool, particle size, shape, angularity, fibrosity, adhesion, hardness, and other properties will be determined on the microscope stage. The simple, rugged atomic-force microscope will image in the submicron size range and has the capability of performing a particle-by-particle analysis of the dust and soil.

Although selected by NASA's Human Exploration and Development of Space Enterprise, the MECA instrument suite also has the capability of addressing the possibilities of life on Mars past as well as future. Rehydrating the Martian soil in the wet-chemistry laboratory will reproduce the conditions believed to pertain to an earlier, wetter Mars. On Earth, the earliest forms of life are preserved as microfossils. The atomic-force microscope will have the required resolution to image down to the scale of terrestrial microfossils and beyond.

Track 2A 4:00

Sahara Campaign for Field Testing of Mars Exploration Instruments for

2001-2005 Mission Rovers

Professor M. A. Mosalam Shaltout

National Research Institute of Astronomy and Geophysics

Helwan, Cairo, Egypt

mamshaltout@frcu.eun.eg

On July 4, 1997, NASA’s Mars Pathfinder lands safely on the surface of the red planet, the first spacecraft to do so in 21 years. After this success, Mars exploration is a high priority program in the United States. There is a plan for testing instruments for a Mars Rover to be launched in the time period 2001-2005 in the Western Desert of Egypt, the driest sahara in the world, and contains a variety of rocks and soil deposited by catastrophic floods early in the history as that occurred in the past history of Mars. Also dust storms occurred for 50 scattered days during the year "El-Kammassen" similar to the dust on Mars. With the planetary society (TPS) in Pasadena, CA, we are currently considering bringing a group of about 12 scientists, 5 from the US (NASA-JPL), 3 from Russia (IKI), 1 from the European Space Agency (ESA) and 3 from Egypt, to do Mars instrument testing in the very dry region of the Western Desert, at three different sites chosen by their analog with Martian desert – like conditions, and contain subsurface water at different depths. The instruments to be tested will be electromagnetic sounder, magnetic coil, infrared spectrometer, radiometer, coordination and GPS Navigation. The exception duration for testing is the autumn of 1998.

Track 2A 4:30

Marsplane

Fabrizio Pirondini

Politecnico di Milano, Aerospace Engineering

Via Lolli 28

I-42100 Reggio Emilia, Italy

pirro@mbox.vol.it

NASA's ERAST program is developing unmanned aerial vehicles (UAV) to fly high altitude, long endurance missions. This paper studies the performances of these aircraft in low Martian atmosphere, an environment very similar to Earth stratosphere. Since no oxygen is available in Martian atmosphere, a solar powered aircraft (i.e. an UAV with solar panels which power electric motors and charge the batteries needed to fly at night) is analyzed. Results show that with current technology, it is possible to develop an UAV capable of continuous flight in low Martian atmosphere. Pathfinder and Centurion aircraft, developed by AeroVironment Inc., could meet that goal without major modifications. Centurion is found to be the best suited to latitude range. Pathfinder, being smaller, could carry less payload and for shorter periods. Flight latitude and season play significant roles in determining payload mass. Such an aircraft could help the first astronauts on Mars to deploy planet-wide weather station and microrover networks, while providing a very detailed picture of soil chemistry and terrain morphology.

 

Track 2A 5:00

Toward Real-Time Global Weather Forecasting

And Atmospheric Climate Retrievals for Mars

Michael Allison (1), Allen Barnes (2), Jennifer Bernell (3), Donna Boccio (2),

Megan McEwen (4), Jeremy Ross (5), Noam Solomon (6), Ina Tegen (4),

and Wei Zhou (6).

(1) NASA/Goddard Institute for Space Studies, pcmda@giss.nasa.gov

(2) Queensborough Community College, (3) Riverdale Country School,

(4) Columbia University, (5) Pennsylvania State University,

(6) Science Systems and Applications Inc.

The upcoming Surveyor98 orbiter to Mars will provide systematic global temperature profiles from a dedicated atmospheric sounder, the Pressure Modulator Infrared Radiometer (PMIRR), for a full Mars year. As a part of our Participating Scientist effort on behalf of this mission, we have

adapted a terrestrial general circulation model (GCM) to the atmosphere of Mars, including CO2 sublimation, diurnally variable heating, and a mature parameterization of upper level wave drag. The simulated zonal-mean circulation over a full Mars orbit shows a polar westerly jet for each

winter hemisphere at the 0.1mb level (approximately 40km altitude) exceeding 100 m/s and seasonally variable equatorial easterlies, nearly vanishing at the autumn equinox. Of particular interest is a consistently simulated 30m/s surface westerly near 30deg south latitude during the

northern winter global dust storm season. We are now using our Mars GCM as a platform for the diagnostic evaluation of various schemes for the retrieval of winds from measured temperatures, including non-linear balance methods. The remarkably similar latitudinal smoothing of potential

vorticity at upper levels for opposing seasons may suggest an important but overlooked constraint on the climatic retrieval of winds from temperatures. Near-term developments of our model include the adaptation of an interactive dust tracer already in use at the Goddard Institute. We will

illustrate the prospects for nearly real-time forecasting at Mars with time-lapse sequences of daily weather patterns.

Track 3A 2:00

One Way and Back: An Introduction to Comparative Missionology

George William Herbert

Retro Aerospace

gherbert@crl.com

Experience with public reception of a prior mission architecture proposed by the author shows that there is poor consensus on why we should go to Mars, and little way to formally categorize the particular goals of a given architecture to compare with other architectures that have been proposed. This paper examines those justifications and goals for sending humans to Mars and proposes a method for comparatively quantifying the target accomplishments of a particular mission. Given such analysis and comparison tools, we can formalize investigations into which exact mission goals are supported and sellable, and thus determine which missions best match the available support.

Track 3A 2:30

Free Return Trajectories for Mars Missions

Christopher Hirata

California Institute of Technology

chirata@alice.caltech.edu

Astronauts on a future mission to Mars will want to be launched on a free return trajectory, that is, one on which the gravity of the Sun and planets alone will return them to Earth in the event of a serious malfunction. Although the total time to travel from Earth to Mars and back is at least two years in free-return trajectories that rely only on solar gravity, this can be shortened somewhat if a Martian gravity assist is used on the return to Earth. For the fall 2011 launch opportunity to

Mars, a mission departing Earth on a 132-day fast transfer orbit to Mars can return to Earth after only 670 days, as opposed to 728 days for the non-gravity-assist free-return trajectory. While this difference of two months in a two-year abort trajectory may seem insignificant, in fact, a return to Earth two months earlier could save the lives of the crew.

 

Track 3A 3:00

Self-Selected Crews for Mars Exploration

Roy Clymer, PhD

5371 Mad River Lane

Columbia, MD 21044-1819

ROY_CLYMER@WRAMC1-AMEDD.ARMY.MIL

Planning for the manned exploration of mars rightly focuses on the engineering issues involved. None the less, given the long duration, close confinement, and anticipated need to deal with unanticipated problems, interpersonal issues may be as important determinants of mission success as engineering ones. Previous models of crew selection are based on a top down model where individual performance is assessed and crews assembled according to performance and political considerations. A new model is proposed wherein astronaut candidates create their own crew teams and one team is selected based on it overall performance in competition with the other teams. It is argued that this will foster improved cooperation, heightened responsibility, lessened interpersonal conflict, and increased willingness to sacrifice, resulting in better overall performance and increased probability of mission success. In addition, such a model lends itself to the specification of additional constraints (beyond required technical skills) on team composition which may markedly increase public support for the mission. (Possible examples include requiring equal numbers of both genders or specifying that no more than one team member can come from any continent or nation.) Finally, it is argued that this model could be compared to present methods experimentally and empirical evidence gathered to decide which model truly results in better performance.

Track 3A 3:30

LOX/Methane Expander Cycle Rocket Engine For Mars Planetary Exploration

Russell Joyner

Pratt & Whitney

Ms 731-95

PO 109600

West Palm Beach, Fl. 33410

joynerc@pwfl.com

This paper is focused on the propulsion requirements of a rocket engine for deep space and planetary missions. Missions to and from mars have received considerable attention over the past few years, in particular missions which would allow the direct examination of soil samples from the planet's surface. This type of mission would provide some insight into the possibility of using the available resources on Mars (e.g. the soil and the atmosphere) to support a strategic exploration plan.

In planetary missions, one of the most crucial concerns is weight. The energy needed to send a payload beyond the earth's orbit is considerable, so the launch vehicle can be very large, and the

propulsion (and cost) requirements quickly become prohibitive. One recent concept which has garnered much attention in the area of Mars exploration is In-Situ Resource Utilization (ISRU). Using ISRU propellants greatly reduces earth launch mass requirements by reducing or eliminating the need for launching return propellants. In fact, ISRU may be necessary to accomplish a Mars sample return mission of any consequence or manned Mars missions, due to the size and cost of

launching a non-ISRU Mars vehicle for those missions.

This paper addresses the use of liquid oxygen (LOX) and methane propellants as the choice for ISRU return propellants. This ISRU propellant option provides the highest performance and has the greatest design experience base. In fact, LOX/Methane provides the highest performance of all the LOX/hydrocarbon fuel combinations.

A simple, reliable demonstrator and operational engine for both ISRU sample return and future more detailed Mars explorations has been conceptualized based on the very mature, highly reliable LOX/hydrogen RL10 engine made by Pratt Whitney. This engine uses the expander cycle and has actually been tested in the past using methane as the fuel and a mixture of fluorine and LOX.

This paper and presentation will discuss the thermodynamic modeling performed, the LOX/Methane RL10 derivative engine concept, the Demo-to-Operational path, and mission sensitivities to design.

Track 3A 4:00

An RLV/Shuttle Compatible Mars Exploration Plan

Kurt Anthony Micheels

Surface Extreme Environment Dwelling Systems

357 Boardman St., #2

Auburn, California 95603

seedsmars@hotmail.com

The non-availability of Heavy Lift Launch Vehicles mandates use of the Shuttle or proposed RLV to transport material for human exploration to LEO. Current Mars exploration scenarios make use of landers and habitats compatible only with HLLV's. The size of the Habitat elements prevents economical delivery to polar test sites or practical use in other terrestrial extreme environments.

A study of technologies was conducted regarding deployment of habitats capable of transport via LC-130H Antarctic logistics aircraft or integration with a robotic lander vehicle with launch to LEO via shuttle or RLV. The result was a logistics support module capable of functioning as an inflatable deployment system. The module design enables Mars landing and surface transport via a robotic rover and facilitates establishment of a surface base derived from the current Mars reference mission.

The module may also be adapted as a deployment system for an inflatable interplanetary habitat integrated with a dedicated transit vehicle.

This paper presents a proposal for a Human Mars Exploration Mission based on the inflatable deployment system and demonstrates how such a system may be derived from Mars Direct/Semi-Direct mission plans.

Track 3A 4:30

A Permanent Moon Base and a Mission to Mars

Alastair Browne

alastair@mindspring.com

In undertaking a project such as a manned mission to Mars, one must take into consideration the technology required for such an endeavor, the length of time it will take, the activities to be performed, and the cost. What is required are efficient transportation systems, long term life support systems, propulsion systems, and efficient means of food production and space habitation. This will take technological advancements we do not yet possess.

One way to acquire the technology for a mission to Mars would be, first, to build a base on the Moon for practice in survival on Mars and for using the Moon as a base to commence the journey.

This paper will cover the prospects of a lunar base for a mission to Mars along with the ways we can obtain this goal. Discussed will be a proposal for a separate way station for Moon bound ships, the categories of Moon bound ships we should develop, the Moon base, its various activities, how the Moon base will expand, and how the Moon can be developed for commercial use. In addition, we will also discuss the mining of near Earth asteroids, their importance in providing for the Moon base the resources the Moon itself lacks, and their potential commercial use along with their benefits. After covering how a solid, scientific, industrial, and self-supporting lunar/space base is set up, this paper will then cover a brief scenario for a mission to Mars, and the first aspects of settling the red planet.

Last to be covered will be allocating funds for this ambitious space program, a newly proposed Space-Industrial Complex, and the prospect for international cooperation. Other space-faring nations have complimentary technologies and finances to our own space program, and working together will benefit all of humanity.

Track 3A 5:00

New Directions: Reevaluating the Lunar Refueling Option

J.D. Beegle and H.L. Beegle

70 Welton Dr.

Plymouth, MA 02360

Recent discoveries in the fields of Planetary Science and Astronautics hold exciting promise of potentially further optimizing future voyages from Earth to Mars. The existence of substantial water ice deposits at the Lunar poles, discovered by the Clementine mission and confirmed by the Lunar Prospector mission, in conjunction with the invention of the Belbruno-Miller Transfer, which significantly reduces the D V required to go from the Earth to the Moon, justify a reexamination of the possible merits of refueling in Lunar Orbit in route to Mars. While the investment in infrastructure required in order to make refueling in Lunar Orbit possible would be so substantial that it would be difficult to justify on the basis of a limited number of flights, if a permanent base or colony is to be established on Mars the synergistic advantages of Lunar refueling become more persuasive.

Track 4A 2:00

Extraction of Atmospheric Water on Mars in Support of the NASA Mars Reference MissionM.R. Grover and A.P. BrucknerDepartment of Aeronautics and AstronauticsUniversity of Washington

The University of Washington has designed an in situ resource utilization system to provide water to the life support system in the laboratory module of the NASA Mars Reference Mission, a piloted mission to Mars. This system, the Water Vapor Adsorption Reactor (WAVAR), extracts water vapor from the Martian atmosphere by adsorption in a bed of type 3A zeolite molecular sieve. Using ambient winds and fan power to move atmosphere, the WAVAR adsorbs the water vapor until the zeolite 3A bed is nearly saturated and then heats the bed within a sealed chamber by microwave radiation to drive off water for collection. The water vapor flows to a condenser where it freezes and is later liquefied for use in the life support system. In the NASA Reference Mission, water, methane, and oxygen are produced for life support and propulsion via the Sabatier/Electrolysis process from seed hydrogen brought from Earth and Martian atmospheric carbon dioxide. In order for the WAVAR system to be compatible with the NASA Reference Mission, its mass must be less than that of the seed hydrogen and cryogenic tanks apportioned for life support in the Sabatier/Electrolysis process. The WAVAR system is designed for atmospheric conditions observed by the Viking missions, which measured an average global atmospheric water vapor concentration of ~2x10^-6 kg/m3. WAVAR performance is analyzed taking into consideration hourly and daily fluctuations in Martian ambient temperature and wind speed and the corresponding effects on zeolite performance.

Track 4A 2:30

Acquiring the Mars Atmosphere using Diurnal Temperature Swing adsorption

John E. Finn, NASA Ames Research Center (1)

K. R. Sridhar, NASA Ames Research Center (2)

The Martian atmosphere has most of the basic ingredients from which the consumable materials needed for exploration activities (life support gases, propellants, structural materials) might be obtained. For most atmospheric processing applications, regardless of scale, the first step is compressing the low-pressure (1% of Earth's atmosphere) gases. Mars' dusty conditions and low temperatures make operation of mechanical compressors troublesome; the enormous cost of electrical power normally needed for their operation makes matters worse. One logical alternative is the use of a device which adsorbs and concentrates relatively large quantities of the mostly CO2 atmosphere at low temperatures, and releases the gas at high pressure when heated. However, even such adsorption compressors can be power-hungry and complicated if they must be heated to high temperatures and cooled with refrigeration cycles.

Over much of the year and across a wide band of latitudes, the surface of Mars experiences a daily temperature swing that is large by Earth standards. For example, data from Pathfinder exhibit a regular swing of about 70 kelvins (200 to 270 K). Laboratory experiments at NASA Ames Research Center indicate that with the proper choice of adsorbent, this temperature swing is large enough to drive an adsorption-based compressor that obtains virtually all of its power from the environment. Depending on the quantity of gas needed, compression ratios can range from tens to hundreds. Such devices would have value for a large number of power-constrained applications, and their designs would be useful for similar units that could produce high-pressure gas on a continuous basis.

We have designed and constructed a prototype of a diurnal cycle adsorption compressor and have begun testing it under simulated Mars atmospheric conditions. In this presentation we discuss the principles of its operation, present preliminary performance data, and describe the larger implications of using adsorption as a technique for compressing and separating Mars atmospheric gases.

Track 4A 3:00

Development of Integrated Petrochemical Manufacturing Facilities on Mars

Sanders D. Rosenberg

In-Space Propulsion, Limited

Darby B. Makel

Makel Engineering Corporation

John E. Finn

NASA Ames Research Center

Local resources on Mars, while not nearly as bountiful as those on Earth, are sufficient to support the development of Integrated Petrochemical Manufacturing Facilities. The presence of carbon dioxide and water vapor in the Martian atmosphere and ice/permafrost and metal oxides on/below the Martian surface hold promise of providing the raw materials required to support the manufacture of oxygen, hydrogen, hydrocarbons, and the generation of solar electric power. The manufacture of these vital chemicals and products derived therefrom, will, in turn, enable the development of a permanent human presence on Mars, followed by the establishment of colonies.

Water (vapor and/or liquid) can be electrolyzed to form oxygen and hydrogen. Hydrogen, in turn, can be used to reduce carbon dioxide to from methane and ethylene. Methane can be used to form ethylene. Ethylene can be used to form other hydrocarbons, aliphatic and aromatic, ethanol, and polyethylene. Ethanol can be used to form polyesters and foodstuffs. Oxygen, water and foodstuffs will be used for life support.

Hydrogen can be used to reduce (hydrothermal reduction) iron oxide present on/below the Martian surface to form iron and water in a closed cyclic process which produces oxygen as a key product. Methane can be used to reduce (carbothermal reduction) iron oxide and silica present on/below the Martian surface to form iron, silicon, and carbon monoxide in a closed cyclic process which produces oxygen as a key product. The silicon will be used to manufacture silicon wafers for solar electric power generation.

Oxygen/hydrogen and oxygen/methane will be used to power local and interplanetary rocket propulsion systems and fuel cells for electric power generation. Polyethylene, polyester, and other plastics will be used to build structures and other parts for Martian bases and colonies, as will metals, such as iron and ferrosilicon. There is no doubt the development of Intergrated Petrochemical Manufacturing Facilities will enable a permanent human presence on Mars, i.e. bases and colonies followed by extensive human exploration of the far reaches of the solar system.

As part of this grand plan, a program is being conducted under contract NAS2-09043 to demonstrate the synthesis of ethylene and other useful products, e.g. methane, benzene, polyethylene, and ethanol, by the reduction of carbon dioxide with hydrogen. These products will be synthesized using inorganic processes based on sound chemical engineering principles. The program is focused on two synthetic paths to produce ethylene in conversion greater that 95%, direct catalytic reduction of carbon dioxide with hydrogen, and catalytic reforming of methane produced by the reduction of carbon dioxide with hydrogen.

Benefits to be derived from the program are: (1) conversion of metabolic wastes to useful products for use on manned spacecraft and planetary bases, (2) the use of indigenous Martian resources for the production of useful products for life support, base construction, and propulsion system fueling/refueling, (3) weight savings which result from reduced on-board supply requirements; (4) production of useful products based on efficient engineering principles, i.e. mass, volume and energy, and (5) reduced resupply from earth which enable economic exploration and colonization of mars and the moon.

The chemistry and chemical engineering processes which were demonstrated on the program will be presented and discussed, e.g. (a) the direct synthesis of ethylene from carbon dioxide and (b) the indirect two-step synthesis of ethylene using water electrolysis and modified Fischer-Tropsch processes. They will be directly applicable to the development of closed life support systems for manned spacecraft, lunar and Martian bases, and , ultimately, lunar and Martian colonies, e.g. the conversion of the Martian atmosphere to methane, ethylene, ethanol, and a variety of polymers for construction and other uses. This may be followed by other interesting syntheses, e.g. polyethylene, a plastic with many varied uses, and ethanol, a potential foodstuff and precursor to polyesters, another very useful plastic

Track 4A 3:30

Producing a Brick from a Simulated Material Theorized to be Found on Mars

for Colonizational Use

David Seymour

266 Vargo Rd.

Horseheads, NY 14845

The goal of reaching and colonizing other planets is coming closer and closer to being realized. One of the problems faced with colonizing another planet is how will we use the resources there to build a colony. Mars is a very likely target for colonization due to many factors, including the abundance of H2O that can be found there

If a colony is to be built, it must be made of something. It would make the most economical sense to use materials found on Mars for colonizing instead of transporting the materials from Earth. It was suggested in a paper by Bruce Mackenzie from The Case for Mars III conference that bricks could be made from the Martian surface for underground structures. My senior thesis is to try to make such a brick.

I have done research trying to determine the composition of the Martian surface. The most important feature for producing a brick was to determine if there were any clays in the Martian soil.

In the same conference, there was another paper by Robert Boyd, Patrick Thompson, and Benton Clark that tried to produce compressed samples of wetted Martian soil which they named "duricrete." Parts of their paper are similar to how a brick would be produced such as adding polymer fibers for additional strength.

The rest of my experiment will be to try to make bricks from researched composition using different ratios of soil to water. Then each of these bricks will be measured for strength and other measurements that seem appropriate once they are formed.

Track 4A 4:00

A Comparison of ISRU Options for the First Human Mars Mission

Kristian Pauly

Institute of Astronautics, Technical University Munich

Exploration Office, NASA Johnson Space Center Houston

The Exploration Office at NASA’s Johnson Space Center is investigating different strategies for the first human Mars missions. The latest results of this work are summarized in the "Design Reference Mission" which is permanently updated as the research continues [1,2]. The mission that is outlined by the design team involves in situ resource utilization not only for the propellant production (ISPP) but also for the production of crew consumables.

In the course of this work, it was the task of the author of this abstract during his work on the Mars Exploration Study Team to make a comparison of all ISRU options that are suited for this task [3,4]. The goal of the six month study was the down selection of the option that is best suited for a human mission out of the countless ISRU options that are proposed. For this purpose, a detailed computer model of 12 different ISRU options was designed, including a number of different fuels (e.g. CH4, CH3OH, C2H4, CO, H2, ...). This model considers not only the features of the core process (e.g. Sabatier) but also the acquisition, filtering, liquefaction, storage and power requirements as well as mission design.

The process data for the computer model thereby is derived more from results of actual systems and less on previous studies. This input to the model is based on the research done by different universities, industry (especially NASA contractors) as well as NASA itself. It is shown that a number of options that look very good on the paper have to be ruled out for practical reasons.

References:

[1] S. Hoffmann, D. Kaplan et al.: "Human Exploration of Mars: The Reference Mission of the NASA Mars Exploration Study Team", NASA Special Publications 6107, July 1997.

[2] B. Drake et al.: "Addendum to the Reference Mission of the NASA Mars Exploration Study Team (V3.0)", NASA-JSC 28208, May 1998.

[3] K. Pauly: "Mars ISRU: Comparison of Options", Interim Report presented to the NASA Mars Exploration Study Team, March 1998.

[4] K. Pauly: "Mars Mission Scenarios Involving In-Situ Resource Utilization", Diploma Thesis, Institute of Astronautics, Technical University Munich, 1998.

Track 4A 4:30

Near Term Economics of Water Extraction from Martian Moons

David Buehler

Guppy Research

buehlerd@itsnet.com

There is a good possibility of water existing locked inside the moons of Mars. This paper examines the economics of retrieving and using water from Phobos. If a system can be designed to extract and transport water back to low-Earth orbit (LEO) economical, it could provide an incentive for non-government investment to fund Mars missions. A water extraction and transportation system is described and the economics of the system are evaluated. The market for water based propellant (either LOX/LH2 or H2O2 with Earth-supplied fuel) is estimated, as well as the costs of various

parts of the system. It appears that the system is economic at current costs. If iceberg-like deposits of ice exist on the moon it could provide competition to water from Mars. The costs of lunar water are estimated and compared to water from Phobos. The system is described in a previous

paper, but briefly consists of a transportation infrastructure based in Earth orbit and a lightweight tanker that meets incoming packages of water and aerocapturing them into Earth orbit. It uses disposable inflatable water containers for the journey from Mars to Earth. A tanker with a

lightweight heatshield meets them individually as they arrive, matching their orbit and transferring the water on board. It uses a UV reflective surface which is heat sunk by the water payload, as well as transpiration cooling system using the water. Splitting the system like this into extraction and aerocapture systems minimizes the amount of equipment which must be flown to Mars.

Track 4A 5:00

A Concerted Action for the Development of a New Rocket Propulsion System

Based on Metallized Propellants

Iskender Gökalp

CNRS

gokalp@cnrs-orleans.fr

A European program is under development with the participation of the CNRS, ONERA, DLR and Russian Laboratories on the implementation of a new rocket engine system which uses a propellant based on CO2 and metal particles, such as magnesium particles. This propulsion system is proposed as a viable concept for Mars sample-return missions, and also as an example for a

generic propulsion concept based on metallized propellants for future launchers. The rational behind the proposed propulsion system is to take full advantage of the concept of in-situ resource utilization for Mars sample return missions, by using the Martian CO2 and magnesium as

propellants. On the other hand, the studies conducted for this objective will also provide useful information for a general use of metallized propellants for future launchers. The project has also a microgravity aspect related to the reduced gravity level on Mars. On the other hand, for

metal particle combustion experiments, microgravity is an indispensable research tool to remove particle sedimentation and natural convection effects, especially under high pressure conditions.

The main objectives of the project are:

i) To determine the ignition limits and the combustion characteristics of

magnesium particle clouds and single magnesium particles during normal and

reduced gravity experiments, in CO2 and for various pressure ranges.

ii) To test a model of a rocket engine using CO2/magnesium powder

propellant and to prove that such an engine can work smoothly and

effectively.

Track 5A 2:00

Yes, But Do The People Support Us?

Humboldt C. Mandell, Jr., Ph.D.

NASA Johnson Space Center

Exploration Office, Mail Code EX

Houston, TX 77058

humboldt.c.mandell1@jsc.nasa.gov

Despite the results of a number of polls, the extent of public support for a human mission to Mars is largely unknown. What would the American people want NASA to do if they were fully informed of what can be done? The NASA Strategic Plan demands a better understanding of what our customers, the citizens, expect us to do. The Administration has called for a new "Dialog with America" to involve the nation more fully in the determination of what their government does in all of its agencies.

To address these issues, NASA has formed a Customer Engagement group, which is actively seeking ways to better communicate with the people, to inform them of what is possible, and to engage them as customers and stakeholders in an organized campaign to promote human Mars exploration. A first step is to find out what an enlightened electorate would want NASA to do.

There have always been polls to measure public attitudes, but, for many reasons, they have had little influence in the casting of public policy in space. A primary reason is that they draw information from an uninformed population.

But there is now new technology for measuring public attitudes, in this case, public support for space exploration. The new methods involve the sampled population actively in the deliberation process. The Deliberative Poll which has been proven in the United States and the United Kingdom, will tell us what an enlightened population would want NASA to do. Deliberative Polls are expensive, and new funding mechanisms have been developed, including a new Foundation for Space Exploration.

The skills required to address these issues do not all exist within NASA. To that end, new partnerships are already being developed with non-traditional sources. The academic community is expected to play a major role.

Track 5A 2:30

Mars, Fostering Public Support

Sam Burbank

234 Dorland Street

San Francisco CA 94114

Many obstacles block any plan to send humans to mars. In conversations on the subject one often feels the discussion has ended before it has begun. Supporters of a human mission to mars often end up preaching to the choir rather than face the questions of an educated and adamant friend or colleague, let alone a stranger. We need to become comfortable, each of us, with discussing and arguing for a Mars mission.

My article focuses on:

Before we can decide on the right plan to motivate the public about Mars, we need to look at why human space exploration ended after the Apollo program; where people lost interest; what it will take to reinvigorate their passion for space exploration, and what brings up such passionate opposition in so many. Some reasons are simple, others complex and unexpected.

It’s important that Mars Society’s objectives remain open. That should be easy. That’s a whole planet next door. Yet time and again we hear people publicly discussing plans for mars as if it were only for a specific group. Yes, the initial years will be tough and in some ways analogous to the American West, but as a selling point that idea is not only uninteresting for many, it’s a real showstopper for some. I don’t try to sell a human mission to mars to a microbiologist the same way I do to a sculptor. They have different hopes for the future, yet neither dream is wrong or less realizable than the other. Anyone willing to dream about a human presence on Mars, about that next step, should be given a wide latitude for their thought of what it might become. The only agreement needed is that it is possible and worthwhile to start now, but then that is the real battle.

Most people don’t know the first thing about mars. Its size of climate; its unique place as the only hospitable neighbor in our solar system. They know about "War of the Worlds," not Olympus Mons; about "Mars Attacks," not Valles Marineris. A little information would go a long way towards helping people understand why it’s mars and not Venus or the moon that has captured our attention.

I’ve talked with people around the would about my hopes for mars and it’s future exploration. I’m thankful to those who were kind enough to tell the overzealous thirty-one year old what thy though of my ideas; those who put the dreamer in his place and made me find them a reason to go. The debate has helped me recognize some of the serious misgivings people have about space travel.

But remember, beneath the apathetic exterior of many skeptics are dreamers who, when their values and hopes can be included and they are shown that this adventure could be unlike any in humankind’s history, can become as excited about Mars as I am.

Track 5A 3:00

Mars Outreach at the Kennedy Space Center Visitor Complex

James E Ball

Chief, Public Services

Kennedy Space Center, Fl. 32899

The visitor center at John F. Kennedy Space Center is NASA’s largest and best attended, attracting more than 2.5 million visitors annually from all over the world. The complex has undergone dramatic improvements and expansions in the past several years, with more than $80 million in user-funded improvements completed or initiated in the past three years alone. The Kennedy Space Center Visitor Complex, recognized last year with the entertainment industry’s highest honor for professional presentation, offers one of the most effective and far-reaching opportunities available for public outreach related to the promotion of Mars exploration.

Mars is already a key component of the message in a variety of current and under-production exhibits and presentations at the Complex. Mars exploration is integrated into current exhibits dealing with human space flight launches, past and present robotic exploration of Mars, feature films, and in-production experiences including a new movie dealing with the search for life, and a walk-through exhibit presenting the relationship between NASA’s robotic exploration of the solar system and future human exploration which will follow. A major new Mars exhibit is in the early conceptual phase. The options for a ride simulation are being explored along with exhibit content displaying technology development in a realistic Mars environment.

This paper describes the methods and purpose of these outreach strategies, and describes plans for a major Mars technology exhibit anticipated in the near future. Partnering arrangements with other NASA centers and Mars researchers will help ensure such an exhibit provides maximum public impact as the issue of human exploration of Mars receives increasing public discussion.

Track 5A 3:30

Mars Needs Guitars!

M. R. Jardin

Dept. of Aeronautics and Astronautics

Stanford, CA 94305-4035

A multi-city tour of rock concerts is proposed as a means to both intensify and focus support for space exploration and to raise money for space exploration research and development, particularly

for Mars exploration missions. Many rock artists are genuinely interested in space exploration as is evident from their CDs, song titles, and performances. If several of these artists are brought

together for a series of performances, the public relations benefit could be substantial as could be the fund-raising potential for specific Mars exploration projects or prize funds. The current popular interest in space exploration, while sometimes paranoiacally misguided, provides a great opportunity to apply this approach to public relations for the space exploration community. This paper describes the type of shows that could be produced and discusses some quantitative aspects of the public relations and fund-raising benefits. Depending upon the caliber of rock artists involved, and the number of shows performed, the number of people reached through advertising and through the news media would be in the range of one to ten million. The range of fund-raising potential is a strong function of many highly-variable parameters and could vary from a few thousand to a few million US dollars.

 

Track 5A 4:00

PLANET MARS HOME PAGE

Selected Observations after Three Years Operation

T. A. Gunn

Transportation Systems Support Analyst

tgunn@myriad.net

Lessons learned about the Web's essential role in funding, design, education and construction of solutions for Mars exploration and settlement are important to the success of the Mars Society for outreach and participation beyond that of previous groups. Although aimed primarily at private sector Mars programs, the implications gleaned from this unique Web site's Email contains important insights for anyone involved directly or indirectly in the quest for Mars Human settlement.

 

Track 5A 4:30

Making it Happen

Jonathan Stabb

NASA, Kennedy Space Center

Mail Stop BC-B

Florida 32899

Mars, by nature is an explorer, an adventurer, and a conqueror of frontiers. Paradoxically, mankind surrounds itself with organizations and institutions which shelter, comfort and protect. Before man sets out on a grand undertaking, he must have the collective will of an institution behind him. Historically, institutions such as the church, or a monarchy provided this necessary backbone for exploration. These organizations provided the broad based "rationale" or reason for the particular exploration, the required resources, both material and labor, and then allowed the explorer to lead the expedition with a single minded vigor. More recently, scientific exploration of our oceans has been successfully accomplished with the organizational support of a private society (Jacques Costeau) and exploration of space through government support (NASA).

This paper shall argue that in order to carry out a successful human mission to Mars, prerequisite conditions of institutional support and singly focused leaders are required. Although the argument will be made with the government in mind as the supporting institution, many analogies could be drawn to a commercial entity acting as the sponsoring institution. The required institutional support does not merely appear. Those with the dream to explore must first engender the support of the general public, align the executive and legislative branches of government, and delineate this exploration as the priority within the "sponsoring" organization (NASA). Although these three areas are loosely tied together, and many times at odds with each other or at odds themselves, they must be aligned. This is primarily a leadership challenge. The second leadership challenge, equally as difficult, is transforming the institutional support, the funding, and existing planning into the reality of operating vehicle and cargo hardware which will successfully achieve the mission.

Track 5A 5:00

Establishing a Human Mission from Planet Earth: Technology Assessment and Social Forecasting of Moon/Mars Synergies

Eligar Sadeh and Evan Valchos

Center for Engineering Infrastructure and Sciences in Space

Colorado State University, Fort Collins

The goal of this paper is to assess the sociopolitical, scientific, and technological dynamics related to the establishment of a Human Mission from Planet Earth (H-MFPE) involving exploration and utilization of the Moon and Mars. This assessment can be accomplished through: (1) understanding the philosophical and epistemological premises of H-MFPE in the context of the significance of exploration in human history; (2) identifying key H-MFPE trends and developments that have shaped the sociopolitical rationale of this effort; (3) articulating the current sociopolitical, scientific, and technological dimensions of the mission by modeling critical variables; (4) examining the range of impacts and consequences related to relevant H-MFPE scenarios; and (5) formulating potential policy options and implementation alternatives through institutional capacity building and broader public involvement.

These tasks are directed at a systematic process of technology assessment and social forecasting to provide a framework for specifying H-MFPE future scenarios. It is suggested that it is too early to plan a detailed, integrated, and long-term program that presupposed human exploration of the Moon and Mars because not enough is known about the lunar and Martian environments or about survivability in long-term space missions required for H-MFPE. Nevertheless, intermediary steps, including the use of planetary probes and the development of enabling robotic technologies for Moon and Mars exploration and utilization, can be undertaken that could make H-MFPE technically feasible. Thus, of critical importance, for s systematic technology assessment framework, are the concepts of robotic/human and Moon/Mars synergies for H-MFPE.

Related to these scientific and technological considerations is the underlying emphasis on policy dynamics which are viewed as inextricably linked to the realization of H-MFPE. In this regard, decision-making and decision support systems, appropriate funding, and international cooperation are identified as "crucial" factors important for the realization of H-MFPE. The paper concludes with a policy utilization analysis that underscores how policy plans for the realization of H-MFPE can be developed through the help of technology assessment and social forecasting by political decision-makers.

8:00 Evening Panel A

THE OLYMPIA PROJECT:

An Inexpensive, Permanent Mars Base Within A Decade*

Roderick Hyde, Muriel Ishikawa and Lowell Wood+ (speaker)

University of California Lawrence Livermore National Laboratory

Livermore CA 94550-0808

An extensively-reviewed program for establishing a permanently-occupied base on Mars on a sub-decade time-scale for a total cost (estimated within ''U.S. Government standard'' models) of the order of $10 billion is presented in some detail.

The Olympia Project aims to exploit current technology in a technologically updated Apollo-esque approach to soft-land on Mars sufficient equipment and materials to support a Mars Base crew of four, including all-Mars-surface rocket- and wheel-based exploration vehicles, life-support supplies sufficient for decade, research equipment and return-to-Earth capabilities for the entire mission-crew. Ways-and-means for indefinitely prolonged mission extension are discussed, as are obvious approaches for strongly leveraging features of the Martian environment for mission enhancement.

Key technologies include flexible-walled structures for the interplanetary transit vehicle and for Martian habitats and vehicles, mission-optimized life-support systems, Martian atmospheric resource exploitation for recovery of hydrogen, nitrogen and oxygen, as well as carbon, and use of generous quantities of photovoltaically-derived energy with which to manipulate usefully the near-Base Martian environment.

Costed major mission options include the full spectrum of life-support technologies, ranging from Apollo-esque one-time use through complete recycling of materials, crew size, Mars system maneuvers (e.g., high-orbit vs. Deimos parking vs. direct atmospheric entry from interplanetary transit trajectory) and Mars-surface mission-richness.

 

Mars as a Suspect for Life

Prof. Bruce Jakosky

University of Colorado

Boulder, CO

There may have been life on Mars in the past; there may be life there today. The author will present the evidence for suspecting the possibility of past or present life on Mars.

 

Mars Airplanes: For 2003 and Beyond

Larry Lemke

NASA Ames Research Center

Moffett Field, CA

Powered heavier than-air craft offer unique potential as tools for Mars exploration. The author has proposed that NASA fly such a vehicle down the slot of the Valles Marineris – the grand canyon of Mars, on the 100th anniversary of the Wright Brothers first airplane flight on Earth.

 

Humans and Telerobots: Together to Mars

Carol Stoker

NASA Ames Research Center

Moffett Field, CA

Mars exploration will require the best capabilities of humans and robots to achieve science objectives. There is a common misconception that robots can explore Mars more cost-effectively than humans. But robots are simply the tools for gathering data for humans. The most effective exploration strategy simply assigns the right tool to the right job. The appropriate tool is dictated by the scale of exploration and the science to be performed. For global mapping involving imaging and composition measurements, orbiters are the best platform. For high resolution observations over regional areas, aircraft are the most appropriate platform. For geological field work, nothing will work better than the human in the field. Robotic rovers will precede human explorers and may augment their capabilities once they are on Mars, but rovers have relatively poor capabilities compared to humans. Field simulations of Mars rover missions have been performed over the last five years which serve to illustrate the capabilities of rovers for performing field science. We also now have the experience provided by the Pathfinder rover Sojourner. The biggest problem for science accomplishment is that the most interesting observations (those immediately obvious to the field geologist) are often missed completely in the rover observations. This holds true even when the rovers are teleoperated in real time in a "telepresent" mode. When teleoperated from Earth, trivial operations (for a human) become major activities. Sojourner, for example, circumnavigated the Pathfinder lander in 90 sols, a task that a human explorer could have accomplished in a few minutes. This talk reviews the lessons learned from rover missions and field simulations and recommends the science strategy for humans and robots together to Mars.

 

 

Friday Plenary Session 9:00

Cultural, Political, and Technical Preconditions for a Human Mars Exploration Program

Dr. Mike Griffin

Executive Vice President

Orbital Sciences Corporation

Friday Plenary Session 10:00

Space Exploration – Just the Beginning

Astronaut John Young

NASA Johnson Space Center

Houston, TX

Friday Plenary Session 11:00

The Mars Pathfinder Mission

Dr. Matt Golombek

Jet Propulsion Lab

Pasadena, CA

Friday Brown Bag Lunch Forum 12:00

Forum - The Race to Settle Mars, Earth having a Baby

What’s it worth to the parent civilization?

Peter Perrine (Moderator)

PO Box 41479

Plymouth, MN 55441

Recent technological breakthroughs in Mars mission design have vastly reduced the cost of birthing a new human habitable world on Mars. Our next president and congress will weigh the value of being the parent civilization that settles Mars. What benefits will the parent civilization get and what are they worth compared to the cost? The question is like asking what the value of a child is to its parents. We will use this parent-child analogy, during this session, to develop a framework to help our leaders think about humanity’s future on Mars. Please come to the session with your own ideas about the benefits of having your own child. Bring your brain, your Case for Mars book, and any papers you may have in this area. Someone bring a calculator, a Mars atlas, and an Earth economic atlas. For each benefit of children, we will list an analog benefit to our civilization of settling Mars. We will then attempt to quantify or characterize the benefits listed to our civilization. The result will be a group paper. It may serve as a primer for a case study for the Harvard Business School and the Kennedy School of Government. It is hoped that this paper as it may be rewritten will serve as an important intellectual foundation for use by our next president and congress as they weigh humanities future.

12 noon

Book signing

Matt Golombek will sign copies of his just released "Mars: Uncovering the Secrets of the Red Planet," published by the National Geographic Society.

Track 1B 1:00

Mars Bonds: a Tool for Private Colonization of Mars

Richard Allen Brown

1248 Institute

202 Ashley Ave.

Charleston, SC 29403

Charlestonideas@hotmail.com

In reading Robert Zubrin's "A Case for Mars", I was intrigued by the possibility of private funding of Mar Colonization. My proposal is fairly simple and easy to understand. There are four parts:

  1. An insurance company such as Berkshire Hathaway would sell $20 billion in Mars Bonds to the public. Essentially, each bond would cost $20,000 and pay no interest over its one hundred-year life. The bond would give the holder the right to 100 square kilometers or about 25 thousand acres on Mars. At the end of the 100-year period, if the bond were not exercised, the holder would receive a return of principal.
  2. The insurance company would invest the money on Earth and promise five per cent per year or $1 billion to fund Mars colonization projects. The insurance company would be looking for low cost alternatives to colonizing Mars with or without the help of NASA or other governmental agencies.
  3. The U.S. based company would have to lay claim to Mars, which would require some rewriting of international law. An appropriate lobbying effort would be needed. Mars colonization advocates could buy shares in the insurance company and leverage that ownership into a lobbying effort.
  4. The privately funded colonization projects would ultimately be successful and the insurance company would trade the bonds for Mars titles. Then the new landholders would pay taxes to the newly formed Mars government. The insurance company would have served its function and the Martians would be in control.

 

Track 1B 1:30

Settlement of Mars: the Mars Lotto

Alex Duncan

Suite ‘P’, 1803 South Foothills Highway, Boulder, Colorado

Given the great number of years involved in this project, I strongly suggest the creation of a lottery to finance the preliminary surveys, etc., plus the actual mission. I believe that state and national governments can be convinced to provide the proper licenses for such a venture.

I propose a monthly or bi-monthly pay-out with substantial cash prizes; in other words, the usual. However, what would be unusual would be that all the winners over a 3-5 year period would enter a separate pool. From this pool, a "grand" prize would be awarded, which would be a spot on the manned Mars mission (obviously, certain physical/age conditions would have to be met). I believe that such a lottery would attract all the necessary dollars to fund the goals of the Mars Society.

This lottery, if sold properly, would be a world-wide operation. Tickets would be sold in every country that allowed the Mars lottery to operate. Let everyone in the world have an opportunity to participate in the exploration of Mars, and possibly other destinations, as well. I think this concept would provide a great deal of positive exposure to the concept of interplanetary travel, which might create additional opportunities for funding.

I understand this is, but one of many ideas on how to raise money. Hopefully one, or more, of the ideas presented will allow this organization to move forward as a privately funded operation.

 

 

Track 1B 2:00

Private Mars Landing: Fast Initial Return on Investment

Edward B. Kiker
21824 Edwards Dr.
Easton, Kansas 66020
kikere@tfs.net

Fast returns on investment from a private mission to Mars should scale into the billions of dollars over and above the costs of the mission.  Even before the mission goes there will be income from sponsoring businesses: the burger and soft drink companies, the computer companies, and others which will want their logos on the mission ships.  Millions of citizens will pay to have their names engraved on plaques to go to Mars.  We must not forget the commercialization aspects for children: the action figures, cereals, model kits, scale vehicles, caps, lunch bags, and other Mars memorabilia. When the mission goes, there will be huge incomes from the advertising sponsors of the stations which cover the mission.  Approaching the planet will generate income from photography of Mars.  Once on the surface the crew can generate early returns from photographs, artists' work, poetry, songs, gems and crystals, fossils, mineral specimens including meteorites, air
samples, and perhaps life forms.  Sufficient materials of value could probably be collected in the first week of surface time to send back by an automated ship for early sale at over a billion dollars.  Scientists may decry commercialization, but governments will protect sources of revenue and
geopolitical stature.  The mission will go.

Track 1B 2:30

An "East India Company" Financing Model for Mars Direct by Creating a Publicly Held Stock company Called: MARS CORP.

John Coston, The Power of Ten Clubs International

3743 Pulaski Ave.

Philadelphia, Pennsylvania 19140

 

MARS CORP. uses a corporate structure as a vehicle to bring the widest spectrum of space supporters into the Mars Direct program. This proposal takes advantage of the long lead-time nature of initial exploration to provide "Demming", just-in-time cash flow programmability.

Problems associated with SEC "Blue Sky" laws are satisfied by utilizing the mutual investment club method.

Corporate structure mimics the democratic process; one share, one vote; providing means of eliminating "politically correct", social engineering from being inflicted upon MARS CORP. via prohibitions written into the bylaws.

MARS CORP. will:

  1. Establish ownership of the first, privately owned, profit motivated, Public Utility on Mars via ownership of the "Zubrin Generators"; and, a commercial "Mars Property Right".
  2. MARS CORP. habitats, for sale to investor/explorers et al, on Mars, will establish a "homestead" private property right, simultaneously creating a claim to land as a homestead right.
  3. Exploration by MARS CORP. rovers will establish a rational claim to "boundaries" of contiguous property claimed by MARS CORP.
  4. MARS CORP. infrastructure, once established, creates extra leverage for negotiating scheduled transport services form NASA et al.
  5. Profit in the highly speculative MARS CORP. is provided Profit Driven Investors via branded merchandise, souvenirs, entertainment contracts, leases, contract services, etc.

Exploration Driven Investors benefit from banking MARS CORP. "credits", on Mars, which will become the de facto medium of exchange. Credits to establish pre-positioned habitats and life support needs.

A Mutual Investment Club program, pre-tested over thirteen years, specifically designed in 1985 by Power of Ten Clubs International, Ltd., a Delaware nonprofit corporation, to enable space supporters of modest means to participate in space exploration will be explained. This concept can fully fund Mars Direct without imposition of economic stress on any participating member.

 

Track 1B 3:00

Private Sector Mars Issues

Wake Up Call for Non-Government Participation

T. A. Gunn

Transportation Systems Analyst

tgunn@myriad.net

Government sponsored Mars programs are very important. However, there are five major groups other than government and government dominated big business that have begun to be players in the quest for Human settlement of Mars. Each of these may be capable of launching their own Mars settlement programs. Must we go our separate ways, or can we work together for a common end result? What role can the Mars Society take to incorporate all groups?

Track 1B 3:30

A Sponsoring Concept for Manned Missions to Mars

Michael Bosch

University of Regensburg, Faculty of Business Administration

Regensburg, Germany

Michael.Bosch@wiwi.uni-regensburg.de

After the first lunar landing in July of 1969, public interest in manned space flight has continue to decrease.

In contrast to this phenomenon. other comparable high technology events, such as international automobile racing, are growing in popularity. Formula 1 racing, in particular, has developed into a highly profitable, privately sponsored economic enterprise.

Because of its tremendous financial power, Formula 1 racing is able to recruit top personnel in the fields of technology, sports, marketing and management. As a result, it is possible to achieve challenging project goals very quickly. Project successes lead to an increase in public interest. Thus, additional private sponsors are willing to put their money into formula 1 events.

This paper starts by pointing out the critical success factors of Formula 1 sponsoring. Next, a number of possibilities re discussed on how to increase public interest in manned space flight. On this basis, a sponsoring concept for manned missions to Mars is developed.

Track 1B 4:00

Entrepreneurial Opportunities from the Colonization of Mars

Keith Parton and Andrew Lawrence

keith_parton@msn.com

pinnacleresources@prodigy.net

Noble arguments have been presented concerning why is advisable and even necessary, to pursue an active program leading to the habitation of Mars. Among these arguments have been the desire to acquire and develop the vast mineral resources available on the planet, the need to rejuvenate the spirit of adventure that was inherent in society during the exciting times of expansion, and the need to keep developing new technology to insure dominance in the global market. This paper will look at the entrepreneurial opportunities one can expect to be developed from an undertaking of this magnitude, and the benefits that will be distributed throughout society.

Little research has been conducted on the benefits from prior space efforts. The public at large generally accepts that the development of new technology took quantum leaps because of NASA’s programs, but in order to win over a dominant segment to support a mission to Mars, a detailed education and marketing campaign will have to be designed to teach the public how the quality of life of each member of society has increased thanks to mans race into space. We will research past breakthroughs in the realms of medicine, education, meteorology, environmental sciences, and technology. We will also highlight how entrepreneurial companies have been able to take advantage of licensing programs and shared technology to the great benefit of society at large. By analyzing historical references on past advances, we will then look forward at some avenues that may be presented in the future for those who are interested in developing the commercial aspects of space exploration.

Track 1B 4:30

Cost Containment for a Thrust into Space

Richard Doranrichdoran@erols.com

We need to explore cheaper methods of research and broaden public interest. Why do we spend billions for research in space? People can only read about it and wish they were the privileged few who get to fly aloft. There are schedule complications, weight restrictions and many limitations.

First, we should attempt an earth based study habitat. (See drawing 1) It is not as grand or spectacular as space, but it is practical.

Second, enhance the research center with a science center. Visitors and students from grade school to college can enjoy these exhibits. This could be a traveling event tailored to an audience for donations. High school presentations will inspire children and improve the future of space.

Third, we should examine practical development. We can develop a basic colonization at limited risk and expense on the moon. The laboratory will ‘impact’ on the moon as an unmanned rover. Remote driving could deliver the rover near a location to meet arriving astronauts. The Delta-X rocket could be used to bring astronauts from a shuttle to the moon and return them to the shuttle. This has potential as a reusable system.

One last thought for our next effort in space exploration and colonization. We should do more development on centripetal gravity. (See drawing 2) This concept will also provide a great ‘Construction Trailer’ for all other future space projects. Mars would be explored from a main craft using the same methods developed for lunar exploration.

This is not the only solution, but I offer one possibility. Public interest increases with involvement. An earth based study habitat can be completed on a two (2) acre area over a four (4) year period.

Track 1 B 5:00

Inspiring The Human Spirit: Why Mars Reality Lags Behind Mars Fiction.

Wil McCarthy

Lockheed-Martin and Science Fiction Novelist

Denver, CO

This paper examines the persistent failure of space devotees to place even one human

being on the surface of Mars. The reasons fall into three broad categories:

(1) That manned space travel is expensive -- REALLY expensive -- and that the people being asked to pay do not see themselves as direct beneficiaries. However, costs do tend to fall as technologies -- particularly materials science and propulsion -- grow more advanced. Eventually the costs may fall either (a) below the public's threshold of annoyance (c.f., Antarctica), or (b) within the reach of private organizations.

(2) That current infrastructure is increasingly geared toward "smaller, faster, cheaper" payloads, whereas manned vehicles are necessarily large, slow, and fantastically fault tolerant. If Mars colonization is a goal, preserving or enhancing current heavy-lift launch capabilities must be a top priority; we must support large, heavy, complex missions as well as cheap, throwaway experiments!

(3) That manned space travel, once seen as an adventure fully in keeping with the American spirit, is now widely viewed as a luxurious boondoggle which diverts resources from both pure science and pure industry. Three reasons contribute: (a) Because Hollywood space travel is both cheaper and more exciting. (b) Because many Americans draw little distinction between real science, fictitious science, and crazy UFO mythology -- in their hearts, few people believe in Mars as a real -- if remote and hostile -- place they could actually visit (c.f., Antarctica, the ocean floor, et. al.). And finally (c) because the Space Race is over, thank God, and oh, by the way, we won. In all three cases, the root problem is the same: space travel as currently practiced and portrayed is elitist, autocratic, and mind-numbingly boring.

With audience participation,. Mr. McCarthy will explore how these obstacles can be overcome

 

Track 2B 1:00

Mars: A Cultural and Scientific History Interactive DVD

Robert Markley, West Virginia University (rmarkley@wvu.edu)

Michelle Kendrick, Washington State University-Vancouver (Kendrick@vancouver.wsu.edu)

Harrison Higgs, Washington State University-Vancouver (Higgs@vancouver.wsu.edu)

Helen Burgess, West Virginia University

Catherine Gouge, West Virginia University

During the past year, we have developed a demonstration multimedia title, Mars: A Cultural and Scientific History, funded by grants from West Virginia University and Washington State University. We will present both a demonstration of the potential of DVD technology (storage capacity: 4.7 GB) for education uses and an analysis of the ways in which this technology radically alters our conceptions of education software. Because of its capacity to combine video, text, and sound, DVD technology offers researchers and students a new range of options in exploring complex problems in interdisciplinary fields, such as scientific education – problems which often require different— and complementary— modes of analysis. DVD technology allows us to include in Mars: A Scientific and Cultural History (MASCH) extensive video clips, animation, morphs, text, voiceover narration, hypertext links to biographies of key figures in the development of planetary research, and an extensive glossary to explain scientific concepts for non-specialists.

MASCH offers in-depth analyses of Mars as both an object of scientific study and a cultural artifact. It includes excerpts of videotaped interviews with Robert Zubrin., President of Pioneer Astronautics and co-author of The Case for Mars; Kim Stanley Robinson, author of Red Mars, Green Mars, and Blue Mars; Martyn Roff of the British Planetary Society and author of Terraforming: Engineering Planetary Environments; Richard Zare, head of the National Science Board; and Tom Meloy, a Principal Investigator on the biological experiments for the 2001 mission, among others. Our format allows students to investigate the social, philosophical, and economic values and assumptions which underlie often different views of the future of Mars exploration and colonization. MASCH offers voice over narration that describes the origins and development of comparative planetology from Percival Lowell to Robert Zubrin while allowing students complete interactivity to access scientific papers, interviews with experts, biographies, bibliographies, and password-only sites on the World Wide Web which include additional archived materials.

The demonstration itself will take no more than twenty to twenty-five minutes, and we will be happy to answer questions about MASCH and DVD technology in general. We will provide our own computer equipment.

Track 2B 1:30

The Frontier of Mars Is an Agriscience Classroom

Larry PayneOroville High Schoollpayne@butte.bcoe.k12.ca.us

Current interest in exploration and settlement of other habitable worlds and the need for a pioneering spirit should be used to create high interest levels in high school students. The best place to start cooperative efforts by space scientists interested in life beyond its current known habitat is with students enrolled in agriscience education. By encouraging the participation of such students in the process of scientific research, there will be a powerful connection established to the next generation of workers. There is a need for scientists to more cognizant and supportive of inclusion of younger people in the process of discovery and establishment of life beyond Earth.

The learning of science by doing science makes the practical application of science a reality in which students experience their own learning. Practical science advanced in western society on the backs of those who worked the land. Agriculture has forever epitomized the evolution of mankind. The development of technologies for the advancement of village societies has been lead by those whose work relates to the soil. Agriculturists have always been, and will likely be, on the frontier of colonization of the land. Civilizations, except for hunters and gatherers, require ecosystem management to survive.

In the program currently under design at Oroville High School, students will approach the study of life, the atmosphere, soils and ecosystems as dynamic systems. However, the primary focus of the program will be on life beyond earth. These will be the first high school students who seek to identify and apply those natural processes which may spread life from this planet to others. They will be encouraged to work with scientists from around the world who are seeking to discover the

requirements of organisms to survive and adapt to ecosystems beyond Earth.

Track 2B 2:00

Teaching from Mars

Gabriel Rshaid
grshaid@marsacademy.com

Since the Martian astronauts are probably now in school, a strong and continuous K-12 Mars education program is essential to foster interest in the younger generations.  In order to be successful and attract the kind of teachers and students that will make a positive contribution to the goal of Mars exploration and settlement, this program will have to based on challenging activities that incorporate the latest technology, including Internet based projects. Additionally, it is  important for local funding at the school level to provide educators with opportunities to interact with real space organizations and corporations. Examples of possible educational activities are :
· Internet based high fidelity mission simulations: Web based role playing simulations where students can become virtual astronauts and mission controllers of a manned mission.
· Chats with scientists: Web chats where students can consult Mars experts on their ongoing projects. 
· Mission outreach activities: Whenever a hitchhiker mission is flown, transmit data over the Internet and let schools receive that data and analyze it cooperatively.
· A Mars Club network: Through an annual membership fee, schools can form their own Mars Clubs, receive posters and other materials and participate fully in all Web chats, projects, etc..
· Teacher workshops: An annual teacher workshop focused exclusively on Mars with featured lectures from scientists and experts.
· A Mars curriculum: A comprehensive written/electronic reference with specific activities, projects and lesson plans for the classroom at all grade levels.
· Contests: Contests that include prizes not just for the students but also for their teachers are wonderful incentives for participation. 
In the author's own experience, space related educational activities are very attractive to the general public and can create media repercussion that can further assist in the objective of gradually communicating the vision of Mars exploration.

Track 2B 2:30

Aresam: Student Concept of Future Mars Space Station

Jonathon Smith and James Bishop

A space station orbiting the planet Mars with the ability to house 18,000 full time inhabitants, equipped with such technology as Fractal Shape Changing Robots and a space elevator. Sound like fiction? Well, it is ..... for now.

Aresam(the name of the station) was designed by a team of sophomores and freshman from Sanilac County, Michigan. The design is explained and detailed in a forty page report, including about thirty pages of typed print as well as drawings and diagrams. It was submitted for competition with other student designs from around the world in the "International Space Settlement Design Competition"(ISSDC). This design placed as one of eight finalists in the competition.

Our report was structured around the ISSDC's RFP, or Request for proposal. It basically required that every team consider the full implications of what a space station required, and to provide for and facilitate those needs. We had to consider many scientific factors such as how to provide food/air/water/fuel for a population of 18,000 people so far from earth, how to power the station, and how to repair it. But we also had to consider many social factors such as how to keep a population of 18,000 people mentally sane 48,000,000 miles from earth, and how to organize the judicial and law enforcement systems for this independent society.

In our design we greatly elaborate on the above and include a limited price estimate, schedule for completion once construction has started, and plan for operation of Aresam. It goes over many major processes and contingencies that this station will use to survive emergencies in space, as well as addressing in depth many of the key technologies that make it possible.

Track 2B 3:00

Growing the Future

Charmin Gerardy

1144 Adams Ave.

Louisville, CO 80027

The quest for Mars depends on the development of attitudes which deem the mission both possible and desirable, and on the training of personnel who are skilled enough and motivated enough to meet the challenges. Education is critical to achieving both goals, and powerful programs can be implemented at even the earliest levels.

The paper describes a program that was used with second through fifth graders in spring of 1997. All aspects of the endeavor were included, form the microbiology of bacterial life to propulsion systems. Students researched, designed, and created transport ships, shuttles, surface craft, habitats, bases, wind turbines, solar energy experiments, working model greenhouse, sewage treatment systems, orbital trajectories, mission parameters and experiment outlines, spacesuits, and even a remote activated, computer controlled rover made of LEGO. In addition, students created diets, calendars, crew selection criteria and biographies, Martian calendars, a sports page for a Martian newspaper that featured appropriate new events, and musical instruments designed form recycled ship waste materials for the astronauts to entertain themselves with. Their work was compiled and presented to the school and parents in a "Marsfest" event, which also featured a guest presentation by Carter Emmart. Other celebrities in attendance include Larry Esposito and Randy Davis of LASP. As an extension of their studies, the students built "reentry vehicles" for an egg-drop that honored the Pathfinder mission, including a detailed model of the lander and rover. The entire exhibit was generously displayed for the summer in the main lobby of the National Center for Atmospheric Research, where it was viewed by thousands of visitors. A reception for the students was thoughtfully provided by NCAR at which students got to discuss their choices of landing sites with a planetary scientist and also had the opportunity to touch a Martian meteorite.

Track 2B 3:30

Our Future On Mars From My Perspective As A 12 Year Old.

Kathleen Bohne

efej19a@prodigy.com

Mars has always been a place of wonder and mystery to earthlings, and the current idea that there could be humans on Mars in less than a decade is, needless to say, an exhilarating and mind-boggling thought. It has been one of mankind's wildest and most dazzling dreams for so

long, and it finally seems to be coming true.

As I am only 12, I could be one of the first people to set foot on the rusty Martian surface. My children could hold in their hands pictures of parts of Mars never seen before, or even pictures of the first crops grown on Mars. My grandchildren could see the first permanent human settlement on Mars and might even live in it. The possibilities seem almost endless with technology progressing at its current rate.

I often wonder what everyday life would be like on Mars. Would things be so alien that everyday activities would become strange adventures? Or would it be relatively similar to life on Earth, despite the obvious differences? Having this in our future is like having the promise of a great surprise yet to come. One that we know is special, vital and completely wonderful, but still ultimately mysterious.

There are major questions, which can only be answered in the decades to come, but we can at least try to lift the veil of mystery about living on another planet by sending humans to Mars. This will be the first stepping stone in the tortuous path to reaching the pinnacle of the human imagination, making another planet our own.

Track 2B 4:00

Secondary Mars Education: Faster, Better, Cheaper

Thomas W. Becker

Consultant Space Education

207-4 Enchanted Parkway

Manchester, MO 63021

tombecker@primary.net

A combination of unique factors has made public education about Mars possible on a far greater scale than ever before. The (1) Information Superhighway, via the Internet and the swift movement of private information, allows fingertip data at the push of a button. This major factor, together with a broad range of (2) up-to-the-minute relay of continued findings by NASA scientists, and the (3) availability of purchasable, subject-targeted CD-ROM disks, allows daily instruction of space-related technology education at a moment's notice.

The question of public school adoption of space technology curriculum, however, still remains unanswered. When, and how, can technology education be infused into traditional curriculum given the strength of the education community's steadfast resistance to any kind of change? Public education curriculum depends upon local boards of education which adopt state and local guidelines. Only through intense public interest in space technologies will boards of education respond to public demands for the kinds of education the public wants. The key to adopting technology education, then, rests with the leaders of industry, education and government.

The ideal solution to these challenges is the adoption of technology education at the state and national levels, from which new policies will filter down to local levels. Other nations already have begun this pathway - Great Britain, France, Canada, Pakistan, to name a few. Other nations are still caught up in the struggle - Brazil, Mexico, India for example. America will be left in the background if public education leaders continue to ignore the nee for space-related education.

The Center for Independent Study at the University of Missouri, Columbia has made some major breakthroughs in space technology education by distance learning. The Center currently offers two high school space technology course, one of which already is on the World Wide Web - "Studying Planet Earth: The Satellite Connection". The second ("Aerospace: Crossing the Space Frontier") will be on the Web shortly, and a third course (" Adventures In Space Science") is being written and will be on the Web next year. All three courses carry a one-half unit science credit.

Track 2B 4:30

Mars Society's Research & Education Center - Design Session

Bruce Mackenzie

BMackenzie@draper.com

What is the Mars Society Research & Education center? We don't know yet, but imagine ...

Your niece the biology student just enrolled for the Mars semester in the closed biosphere. The whole class will follow "Mars time". Your nephew is competing in its contest to build the best Mars vehicle. Engineering schools are competing in the 2nd Mars habitat contest

there, to build buildings with the least possible material "brought from Earth". Last year's winning building is now the Mars Society headquarters, others are used for visitor lodging.

The new US president & NASA agreed to support a long-term Mars environment simulator there, big enough for testing a complete 4 person Mars base. Even your neighbor had her submission included in the "Recipes for a Small Red Planet" cookbook published by its restaurant.

You finally succumb to curiosity, and schedule the "Mars weekend" in your vacation plans: After a short ride from the Denver airport, you arrive at what appears to be Von Braun's 1950's Mars rocket high on a ridge. Ignoring the gift shop, you join your 'crew' boarding the rocket. It's large wings frustratingly obscure the valley beyond. Next comes the Virtual Reality launch, quickly followed by approach to Mars. (The interplanetary coast is omitted.) At last, you open the other hatch, and catch your first view of "Mars-Ville", beyond the ridge. (Officially known as the Mars Society

Research and Education Center.) ...

What will it look like?

...We don't know, because it is to be designed at this session of the Mars Society Founding Convention. You may contribute in advance one viewgraph of a building or funding

suggestion you would like included.

Track 2B 5:00

Mars Educational Resources - Nuts and Bolts and the Higher Country of the Mind

Donald M. Scott

NASA-AESP

NASA-Ames Research Center

Moffett Field, California

During the past 25 years, much work has been done to prepare humankind for Mars. In technical, scientific, and economic terms, we are pretty well prepared to go, to explore, and to return. bUt a major Mars preparation task needs more attention. This is the education of the "Mars Kids", the children now in school who will design, fund, and conduct the human missions to Mars.

The first Martians currently attend school here on Earth. A good education will be the foundation for their successful missions to Mars. This is even more true if we seek to develop the most efficient and cost-effective human missions. Teachers of the Mars Generation need resources to help them with the job.

One such resource is a new way of thinking, along the lines described by NASA's Jesco von Puttkamer: "…a new frame of mind that shifts the emphasis from individual subjects to the interactions and relationships between them." Another resource is the set of nuts-and-bolts materials available to teachers who would prepare the Mars Kids.

The paper discusses the new interdisciplinary way of thinking. It also presents a model for interdisciplinary learning called the Geo. S Paradigm. Finally, this paper provides brief information about nuts-and-bolts Mars Education resources.

Track 3B 1:00

Greenhouse Models for Terraforming Mars

Chris McKay

NASA Ames Research Center

Moffett Field, CA

Using artificially produced greenhouse gases, it may be possible to warm Mars to habitable conditions.

Track 3B 1:30

Ecosynthesis on Mars - The Problem of Water

Dr. Julian A. Hiscox

IAH Compton Laboratory

Julian.hiscox@bbsrc.ac.uk

The most likely candidate planet in the solar system for planetary engineering using near term technology is Mars. It is second only to the Earth in terms of biocompatibility for terrestrial life, and lies within the habitable zone. However, the Viking Mission clearly demonstrated that at the Viking Lander sites, and by inference the rest of the planet, the Martian surface environment is effectively sterilizing for all forms of terrestrial organisms. In addition the surface of Mars is devoid of liquid water - a prerequisite of life. To render Mars habitable, the primary objective will be to increase the atmospheric pressure, thus increasing the mean global surface temperature and enabling liquid water to exist. The two main sources of water on Mars are thought to be the north polar cap and the regolith. The quantity of water on Mars is uncertain, and estimates range in order

of magnitude, equivalent to a layer of water over the planet: 13 to 100

meters deep.

Biology will play a major role in both the planetary engineering process and in the stabilization of the resultant climatic system. Pioneer microorganisms and subsequent generations will provide a pyramid of biomass for successive generations of organisms to metabolize, provided the relevant organisms can grow on Mars. Based upon terrestrial experiments the growth of such organisms on Mars can be modeled. To avoid unnecessary energy expenditure the introduction of pioneer

organisms and ecosystems on Mars will have to follow the release of liquid water, which is likely to progress from the equator to the polar caps. Unfortunately, most of the water on Mars is thought to be contained pole-wards of 40 degrees of latitude. A simple model suggests that although equatorial regions will become habitable from a temperature point of view, liquid water will be limiting.

Track 3B 2:00

Physiological Ecology of Terrestrial Microbes on a Terraformed Mars

James M. Graham

Linda E. Graham

University of Wisconsin

Madison, WI 53706

The present climate of Mars is characterized by a number of environmental factors that are so extreme they preclude colonization by terrestrial microorganisms. These factors include low average surface temperature (-60C), diurnal temperature ranges up to 100C, intense UV

radiation (7x103 ergs.cm-2.s-1) and an atmospheric pressure so low (6-7 mbar) that liquid water is not stable on the surface. Conversely, light levels (max of 860 5mol quanta.m-2.s-1 PAR) are adequate for photosynthetic microbes, bryophytes and many flowering plants. Temperatures in the

southern hemisphere are adequate for Antarctic cryptoendolithic microorganisms even now. Moisture levels in the Martian regolith (1-3%) are comparable or greater than those in terrestrial deserts, and the regolith may contain sufficient nitrates to support microbial growth. If the average surface temperature and atmospheric pressure could be raised by such planetary engineering processes as solar mirrors and greenhouse gases (Zubrin and McKay 1996), terrestrial microorganisms could be implanted on the surface of Mars. If pressure rose to 90-300 mbar,

diurnal temperature ranges would decrease, and liquid water would be stable. UV radiation would remain a serious limiting factor, but hardy bacteria, lichens and cyanobacteria could survive under rocks or beneath their surfaces. Generation of about 2 mbar of O2 in the atmosphere could

create enough ozone to shield the surface from UV radiation (Fogg 1995) and permit a more diverse assemblage of microbial colonizers. Algae and cyanobacteria can grow at high levels of CO2 and generate their own O2 for respiration. They can survive low O2 periods by switching to various anaerobic metabolic pathways. Initial nitrogen cycling would be largely microbial metabolism of regolith nitrates, and recycling of organic nitrogen and ammonia. There appear to be few obstacles to establishing a microbial biosphere on Mars

Track 3B 2:30

An Ecological Approach to Terraforming, Mapping the Dream

Richard W. Miller
University of Waterloo, Canada
mars@kw.igs.net

James Lovelock’s Gaia hypothesis, suggests that Earth’s biosphere is a self-regulating entity with the capacity to keep our planet healthy by controlling the physical and chemical environment. Central to Lovelock’s model are the ideas of interconnectivity and feedback between components of the biosphere, and that life, when viewed on a global scale, has emergent properties. In effect, the Earth, its atmosphere, oceans, rocks and life comprise one entire ecosystem. According to Eric D. Schneider, Hawkwood Institute and James J. Kay, University of Waterloo, ecosystems are systems of organisms, interacting with one another, within spatial and temporal boundaries, and consist of processes which bind organisms together and influence the development, structure and function of the ecosystem. They view ecosystems as "evolving complex systems that are held away from thermodynamic decay by imposed physical or chemical gradients." The Earth, as far as we know, is the only existing planetary ecosystem. The physiognomy of planetary engineering is generally considered to have two aspects: ecopoiesis and terraforming. The goal of terraforming Mars would be to create an uncontained planetary biosphere emulating all the functions of the biosphere of Earth, one that would be fully habitable by humans.
So far, much of the speculation on planetary engineering has concentrated on the physical and chemical modifications required for terraforming Mars. This work has been based on traditional analytic and reductionist approaches to scientific inquiry. Silvio Funtowicz, Institute for Systems, Informatics and Safety, and Jerry Ravetz, Research Methods Consultancy, Ltd. claim that these methods are inadequate to cope with dynamic, complex systems, such as ecopoiesis and terraforming, which are characterized by unpredictability, incomplete control, and a plurality of legitimate perspectives.  Terraforming, in which humans are an integral component, is an ‘emergent’ complex system which includes properties of reflection and contradiction. In this paper, I examine methods for describing complex systems, the tools which can be employed to manage them, and then suggest how these ideas can be applied to terraforming.
 

Track 3B 3:00

Terraforming Mars - Reactivating the Hydrosphere

Patrick Whittome

6E South Lodge

China World Apts

China World Trade Center

Beijing, China 10004

Shell Companies in North East Asia

 

 

The first steps towards terraforming Mars and ultimate utilization of Martian water resources will be most effected by three determinants:

1 .The surface is very cold and very dry and has a minimal atmosphere

2. The planet's interior is relatively much hotter and is assumed to contain liquid water.

3. Some water is frozen solid on the surface (e.g. at the pole but most is locked underground in permafrost layers at or near the surface or in liquid form at greater depths.

All solutions for reactivating the hydrosphere are solutions for directing energy at the surface and / or subsurface. I would like to discuss an extra technique to add to mirrors, greenhouse gas production or violent nuclear release of volatiles, which I jokingly call: Hot rusty snow!

An enormous indigenous reserve of energy to melt the ice caps (water or CO2) and to release CO2 from the regolith is already present on Mars in a usable form - the geothermal heat in the deep subsurface. The objective is to use drilled wells as channels for the transfer of heat and water from the subsurface to the surface areas.

Track 3B 3:30

Terraforming & Landscape Architecture

Mark R. Northcott

Landscape architects currently plan and design the environments in which we will live in the future. Every day enormous amounts of foliage are removed from entire regions. Every year more and more natural resources are mined for energy and processed back into the soil or atmosphere. Huge quantities of landmass are constantly reshaped and fertilized over and over again to make way for an increasing populace. Each act above is done to make our planet more habitable for us. It is only a natural professional step in a progressive direction for some in the field of landscape architecture to expand their practice to include the possibilities of establishing sustainable environments on other planets.

If we are to travel to Mars there will come a need to extend their presence on the Red Planet for longer periods of time. It will become the responsibility of the profession to remain on the ‘cutting edge’ of current technology and public interest. There will then come a need to protect future colonists from the harsh and merciless conditions of the Martian atmosphere. Considering long-term study and colonization on Mars means that serious thought be given to the idea of terraforming Mars.

"…drastic improvements in the life-sustaining characteristics of the environment of the red planet may be effected by humans using early to mid-twenty-first century technologies." (Schmidt, Zubrin. 1996. P.144)

We may never see the results of a terraformed planet, but we at least may hold the vision, initiative, and hard work to see the beginning of a magnificent transformation of the red planet.

"Moreover, in the process of modifying Mars, they are certain to learn much more about how planets really function and evolve, enough perhaps to assure wise management of our native planet." (Schmidt, Zubrin. 1996. P.145)

Track 3B 4:00

Terraformation of Mars

Charles Hancox

5260 Blackcloud Loop

Colorado Springs, CO 80922

The literal meaning of terraformation can be described by dividing the word into parts: terra--the earth, and formation--the process of giving form or shape. There is not as of yet a universal definition of terraformation, but it can be described most generally by the following definition:

"Terraforming is a process of planetary engineering, specifically directed at enhancing the capacity of an extraterrestrial planetary environment to support life. "

The ultimate in terraforming would be to create an unconstrained planetary biosphere emulating all

the functions of the biosphere of the earth--one that would be fully habitable for human beings.

The purpose and long-term goal of space exploration should be to permanently establish the human presence into space and to make conditions necessary to permit new civilizations to grow and prosper independently from the Earth. Migration and colonization to hostile environments have been traits of biological evolution for billions of years. A recent letter to the editor of Space News titled "Meaning of Life" expresses one reader's point of view: "We should be going to Mars not mainly as paleontologists, but as pioneers. We should be going to Mars not to learn about its past, but to understand its prospects for our future."

The major steps to fully complete terraforming Mars consist of the following: raise planet surface temperature, raise atmospheric pressure, make the surface wet, change atmospheric chemical composition, and reduce the surface flux of ultraviolet radiation.

The utmost treasure with a terraformed Mars is the birth of an independent space-faring civilization and the opportunity to expand human ingenuity. A colossal endeavor such as terraforming Mars will require an undivided global commitment. It may be opposed as a skeptical, exploitative undertaking and will certainly face several ethical, political, and legal barriers.

_______________________________________________________________________

REFERENCES: Fogg, Martyn J. Terraforming: Engineering Planetary

Environments. Warrendale: Society of Automotive Engineers, Inc., 1995.

Liss, Jeffrey G. "Meaning of Life." Commentary: Letters. Space News (Sep

9-15, 1996) Vol 7 No. 35:14.

s

Track 3B 4:30

Cryptoendolithic Microorganisms as the Chemolithotrophic Alternatives toPrimary Terraforming Colonizers on Mars.

Dennis Ray Schneider

P.O. Box 958

Round Rock, TX 78680

drdiver@mail.utexas.edu

Terraforming strategies may be divided into primary, secondary and tertiary stages. These stages have generally focused on photosynthetic microorganisms as primary colonizers of the Martian surface. The ability of any microorganism to tolerate Martian surface conditions is past the limits

tolerated by any known microorganism. Even inferred properties from studies of extremophile physiological properties suggests that finding a successful primary colonizing microorganism, microorganisms, or ecosystem would be difficult. A more likely successful candidate site for primary colonization would be within rock or below the Martian surface. Protection of initial

colonizing microorganisms from temperature extremes, surface oxidants, and greater likelihood of available water are some of the benefits from using subsurface environments. The use of chemolithotrophic microorganisms offers the possibility of using the reducing power in metallic or ferrous iron (or other potential electron donor minerals) for carbon fixation and development

of microbial ecosystems based upon this system of primary production. These systems are analogous to those known to exist in the terrestrial subsurface. The use of such "privileged sites" for initial colonization may provide the biologically derived materials which would increase the likelihood of success for using endolithic cyanobacteria such as Chroococcidiopsis in similar protected sites to begin secondary colonization of the Martian surface.

Track 3B 5:00

Preparations for a Post-Colonial Mars

Rudy Behrens

Philadelphia, PA

While we may debate the early stages of Mars colonization and argue if it will be a scientific outpost, or a mining operation or in some other way tied economically to Earth, we all agree that the ultimate goal is to make Mars a new habitat for humanity. We all look to the day when there will be a free Mars, able to exist without economic ties, or justification, with Earth.

As history shows, most new territories have been settled by farmers looking for a place to call their own. I believe this will also be the case for Mars, though for some considerable time into the future, Martian farms will be some kind of controlled and/or artificial ecosystem. Perhaps they will be so simple as to only provide food for the inhabitants and a few others nearby. However, terra farmers do not have the skills to be Martian farmers. Martian agriculture must move beyond the biologists, botanists, engineers and other technical professionals and become the trade of career farmers. Where can such farmers come from?

The same technologies can also be desirable on Earth. Our present methods deplete soil and are dependent on petroleum based fertilizers. We at Aurora Farms have developed a semi-closed ecosystem form of agriculture that is actually cheaper, and more efficient in use of resources, than field agriculture. Currently we are constructing these systems in city environments and selling the food profitably. We believe the children and grandchildren of these urban farmers will be the first Martian sodbuster. Having grown up in such an environment, they will possess the skills and instincts to grow food successfully on Mars.

The paper will describe the process in greater detail and demonstrate how the skills used will be transferred to a Martian environment.

Track 4B 1:00

Nuclear Thermal Rocket - An Established Space Propulsion Technology

Stanley V. Gunn

20360 Tau Pl.

Chatworth, CA 91311

The Rover and NERVA programs, sponsored by the Atomic Energy Commission, U.S. air force and NASA during the period 1956 through 1973, were focused on the applied research, development and demonstration of nuclear fission-powered rocket propulsion systems. Initially, the U.S. Air Force's potential applications were those requiring the delivery of very heavy [payloads to intercontinental objectives; but, in 1958, NASA assumed the mission definition responsibility and designated first the utilization of the NTR as an alternate upper stage propulsion system for the Apollo program and later as the leading propulsion candidate for manned-Mars missions.

The depths of the programs were substantial; major test facilities were constructed at Site 400 of the AEC's Nevada proving grounds, and supporting component and subsystem test facilities were created at LASL and Rocketdyne for the ROVER program, and at Westinghouse and Aerojet for the NERVA program. Reactor fuel element technology, focused first on hexagonal graphite elements and then on composite and carbide-based elements, was created, which subsequently resulted in fuel element gas-exit temperatures of 3100 K. In addition, high pressure- high volume rate liquid hydrogen pumping systems were created for the conduct of the planned reactor (ranging to 5000 megawatts) and engine tests (ranging to 1100 megawatts/50,000 lbs. thrust) at Site 400. A significant benefit of the liquid hydrogen pumping technology, developed under the ROVER program, was its direct adoption to the liquid hydrogen pumps utilized in the J-2 engines of the Apollo program's Saturn V launch vehicles. Also, the projected heat loads (greater than 25 Btu's/sq. in.) on the integral coolant channels of the reactor assembly's high expansion thrust nozzles were satisfied by the utilization of advanced coolant design concepts and materials. Finally, the design and development of new, radiation-resistant reactor-engine system control components was accomplished. IN all, 19 reactor/engine hot tests were conducted with the demonstration of the versatility and practicality of nuclear thermal rockets. This experience based resulted from the assembly and utilization of a remarkable pool of scientists and engineers, and the expenditure of $1.4 billion 1960 dollars.

After definition of the 1st generation NERVA Engine, the technology developments of the ROVER program were directed toward performance and reliability upgrades that would support improved design objectives for the 2nd generation engine. The upgrades achieved will support engine Isp of 900 sec., engine thrust-to-weight ratios up to 10:1, and engine full power life of 1 to possibly 10 hours, while permitting up to 60 restarts. IN addition, such engines are blessed with controlled throttle ability from full thrust down to nearly zero thrust. Because of core diameter-criticality considerations, the realization of the 10:1 thrust to weight ratio depends in part on the selection of design power of the engine's reactor (35 in. diameter core) to be at least 1500 mw (75,000 lbs. thrust), although design power levels down as low as 500 mw can be engineered, with some penalty in engine specific weight. With demonstrated fuel element power densities ranging as high as 1.3 megawatts/fuel element, it should be possible to generate 2,500 megawatts (125,000 lbs. thrust) utilizing a 35-inch diameter core. The ease with which such future reactors and engines might be developed is dependent on the restoration and modernization of appropriate test facilities. Preliminary analyses have shown that it is practical to completely contain, and re-liquefy for reuse (along suitable scrubbers), the hydrogen consumed in full-power, full duration hot test.

The technology of the ROVER and NERVA programs remains completely relevant to the propulsion requirements of possible, near-term (out to year 2020) human exploration-Mars mission. It may also offer a realistic basis for NTR engines designed to support other demanding space exploration missions within our solar system. A critical consideration, however, is the retrieval and conveyance of this technology and relevant test capabilities to the scientists and engineers to be recruited for such programs.

Track 4B 1:30

Fission Rockets for Advanced Space Exploration

Michael G. Houts, David I. Poston, and Deborah R. Bennett

Los Alamos National Laboratory

Los Alamos, NM

R. J. Lipinski, S. A. Wright, R. X. Lenard

Sandia National Laboratories

Albuquerque, NM

Thermal rockets that utilize a fission energy source (also known as nuclear thermal rockets, or NTRs) could enable routine access to most areas of the solar system. Near-term systems could enable rapid, manned access to Mars and the main asteroid belt. More advanced system could enable routine access to the outer planets.

This presentation will discuss three NTR systems: the Rover rocket that was developed to the stage of full ground tests in the 1960s and early 1970s, a particle-bed rocket that was researched in the 1980’s and early 1990’s, and a gas core concept on which some research has been performed.

 

Track 4B 2:00

Nuclear Electric Propulsion Architecture

For Human Mars Exploration

R. X. Lenard, R. J. Lipinski, S. A. Wright

Sandia National Laboratories

Albuquerque, NM 87185

M. Houts, D. Poston, D. Bennett

Los Alamos National Laboratory, Los Alamos, NM

The advent of the highly publicized Mars Global Surveyor and Mars Pathfinder missions has renewed interest in Mars exploration. Numerous architectures have been proposed to accomplish a human exploration mission. The Synthesis Group base-lined a 30-45 day surface mission utilizing nuclear thermal propulsion as a mechanism to perform the Trans-Mars Injection burn and also for earth return propulsion. More recently, the NASA Design Reference Mission has base-lined a bi-modal nuclear thermal stage with a small (~30 kWe) power generation capability. The Mars Direct architecture proposed by Zubrin, employs a series of heavy lift launch vehicles using conventional propulsion to transport the crew direct to Mars.

Only infrequently are all-electric propulsion architectures proposed, typically because they do not deliver the high thrust needed for short crewed-transit to Mars. This limitation can be overcome by using electric propulsion to transport massive elements to a highly elliptical orbit or to nearly a C3=0 orbit about earth, and subsequently have crew join the ship in the light-weight Mars descent vehicle. Then a small chemical propulsion system provides the small additional delta-V needed to achieve Trans-Mars Injection TMI velocity. This is the so-called hybrid approach.

This architecture has much to recommend it. It can be argued that this architecture provides the greatest mass to Mars for the minimum overall program cost. It dovetails quite well with potential commercial uses of nuclear electric propulsion. Further, it can reduce or eliminate the need for development of a new heavy lift launch vehicle. Since the Space Shuttle, no new launch vehicle has been deployed. Even the Evolved Expendable Launch Vehicle program is merely an upgrade of existing vehicles. The attraction of the hybrid architecture is that it minimizes cost, trip time, and dependence on a new launch system, arguably the highest risk element of human Mars exploration missions.

Track 4B 2:30

Manned Missions to Mars with the Gasdynamic Mirror

Prof. Terry Kammash

University of Michigan

A novel concept is presented for combining magnetic and gas-dynamic effects to confine a reacting thermonuclear fusion plasma. Such a device could provide a large and efficient space power source, potentially enabling fast human round trip missions to Mars.

Track 4B 3:00

Exploration of Mass-Based Alternative Propulsion Systems

Amanda J. Gilbert

Stanford University

dixee@leland.stanford.edu Since May 1997, an international collaboration has been exploring the possibility of using mass-based systems as an alternative to rockets for space travel. Claims of working inertial propulsion have been made many times, but have not withstood rigorous testing to the point that

such a drive could be in a spacecraft. The current project, centering around a public-domain technology invented by David E. Cowlishaw of Silverton, Oregon, has yet to prove or disprove the possibilities of such technology, but is in the process of building and testing numerous models

utilizing a mass-based system.

For any claim of inertial propulsion, a test should be conducted that determines whether a system can propel itself against the force of gravity for an extended period of time without supplemental lift provided by rockets, airfoils, etc. Such a system, a demonstrable "self-lifter", is the primary goal of the project. The possibility of the system working in the absence of gravity has been debated, and as such, if the primary goal of the project is accomplished, a secondary goal of the project is to

determine whether it is feasible or even possible to successfully deploy the system in the absence of a strong gravitational field. An additional consideration is the relative efficiency of such a system. Because the technology currently under investigation is a means of directing thrust, the amount of energy required to operate such a system is critical to its success. A highly energy intensive system could limit the technology to longer distance flights where using rockets would be prohibitively

difficult or expensive. The project leaders expect to answer these questions conclusively within the next three years.

Track 4B 3:30

FRC Fusion Based Rocket Propulsion: Mars in Three Weeks?

Tony Rusi

Seattle, WA

earthflight1@yahoo.com

Recent advances in Field Reversed Configuration Fusion Propulsion indicate that a sustained research and development program on the order of five years culminating in on-orbit testing of an FRC fusion propulsion rocket could lead to the type of improvement in plasma temperatures seen in tokamak research programs since the seventies. Advanced aneutronic fuels indigenous to the lunar and Martian surface could provide the profit incentive to make mars colonization feasible

if coupled with land grants. The vastly reduced trip times could drop the cost of a sustained colonization program into a range approachable by private enterprise.

Track 4B 4:00

ESCORT: a Pratt & Whitney Nuclear Thermal Propulsion

And Power System for Manned Mars Missions

Claude R. Joyner

Pratt & Whitney

Ms 731-95

PO 109600

West Palm Beach, Fl. 33410

joynerc@pwfl.com

The purpose of this paper is to describe the conceptual design of an upgrade to the Pratt & Whitney ESCORT nuclear thermal rocket engine. The ESCORT is a Bimodal engine capable of supporting a wide range of vehicle propulsive and electrical power requirements. The ESCORT engine is powered by a fast-spectrum beryllium-reflected CERMET-fueled nuclear reactor.

In propulsive mode, the reactor is used to heat hot hydrogen to approximately 2700 K which is expanded through a converging/diverging nozzle to generate thrust. Heat pickup in the nozzle and the radial beryllium reflectors is used to drive the turbo-machinery in the ESCORT expander cycle. In electrical mode, the reactor is used to heat a mixture of helium and xenon to drive a closed-loop Brayton cycle in order to generate electrical energy.

The original ESCORT design was capable of delivering 1000 lbf of thrust at a vacuum impulse level of approximately 900 sec. Design Reference Mission requirements (DRM) from NASA Johnson Space Center and NASA Lewis Research Center studies in 1997 and 1998 have detailed

upgraded requirements for potential manned Mars missions. The current NASA DRM requires a nuclear thermal propulsion system capable of delivering total mission requirements of 45000 lbf thrust and 50 kWe of spacecraft electrical power. This is met assuming three engines capable

of each delivering 15000 lbf of vacuum thrust and 25 kWe of electrical power. The individual engine requirements were developed assuming three out of three engine reliability for propulsion and two out of three engine reliability for spacecraft electrical power. The approximate target vacuum impulse is 925 sec.

A system integrated performance methodology was developed to assess the sensitivity to weight, thrust and impulse to the DRM requirements.

A trans-Mars injection mass sensitivity to both number of engines and thrust showed that an ESCORT baselined to a thrust of 15000 lbf at a vacuum impulse of 911 sec best addressed the NASA DRM requirements. The paper discusses the conceptual design and the application to the new design reference missions.

Track 4B 4:30

Human Mars Mission Architecture Assessments

Benjamin Donahue

Boeing Aerospace

M/S ZA-06

555 Discovery Dr.

Hunstville, AL 35806

benjamin.b.donahue@boeing.com

This paper reports on an assessment that was done by the Boeing company of a variety of alternative approaches to piloted Mars mission. On the basis of both cost and risk, nuclear propulsion was found to enable the preferred mission options.

Track 4B 5:00

High Orbital Microgravity Environments (HOME)

Bryan Palaszewski

NASA Lewis Research Center

bryan.a.palaszewski@lerc.nasa.gov

As part of the International Space University (ISU), a design project was conducted to plan future space utilization. The project outlined and designed a family of high orbital microgravity environments (HOMEs), or a wide variety of space habitats and platforms, where each HOME would focus their energies on different and specific space technologies and terrestrial needs. A family of HOMEs would provide orbital havens for new budding industries, micro- and nanotechnology applications development, manufacturing research, Earth and space observation, biomedical research, and any other space related discipline. The HOME would use the space

environment for its many highly valued qualities: nearly continuous sunlight, microgravity, and the flexibility to use any area (location, orbit, Libration point, etc.) in space to create the most optimal

environment for the HOMEÆs dedicated task.

The current difficulty with space flight is the high cost of access for getting into orbit, and the costly planning and execution of space projects. A low cost method of space access and utilization will open new markets and create new wealth-generating products for all nations. The HOME

project would include all of the local technical disciplines of any nation, the manufacturing capacities of the its economy, the universities, and the health and services technologies for telemedicine. Space propulsion, combined aeronautical-space vehicles, combustion, fluid mechanics, communications, electronics, structures, materials, and facilities developments would all be uplifted by the basic and applied research conducted in orbit. A HOME can produce space power for remote sites, bolster the economies of emerging nations, and anything else you like.

Transportation to and from the orbital economy with expendable or reusable launch vehicles would be an integral part of the HOME project, as well as the ground resources to feed the orbital economy. Planetary HOMEs on and near Mars are likely candidates for the future development of planetary resources and human settlements.

Track 5B 1:00

Mars Together, When and How

Bruce Lusignan

Center for International Cooperation in Space

Stanford University

Stanford, CA 94305-4053

It has been five years since Stanford published a comprehensive study of an "International Mars Mission." That and two other studies by Bob Zubrin and by NASA's JSFC identified ways to explore Mars at far less cost than original estimates of earlier Space Exploration Initiative studies. What is the status today?

The Stanford study used a conventional heavy lift vehicle, the Russian Energia. Eight launches were needed in the "split architecture" mission. Two to pre-supply surface equipment for habitat and exploration. One to land and return the crew to Mars orbit. One to store Earth return fuel in Mars orbit. Two for the crew's vehicle. Two more cargo flights of return fuel and surface supplies serve as back up and pre-supply for a second visit.

The Stanford design emphasized use of existing technologies, non-nuclear power systems and international participation to reduce costs and increase to cooperation.

Today, discovery of evidence of early life forms in Mars meteorites and surface pictures from Sojourner have kept public interest alive. Nuclear space power is more distant, more expensive and less popular politically. International cooperation on MIR and the International Space Station continues despite a skeptical press. Private sector SSTO initiatives to replace the Shuttle show promise, even greater promise if they can capture the world's space exploration market. The Stanford International Mars mission is easily modified to use "Space Tugs" deliver to Low Earth Orbit by SSTO's in place of Energia. Mars exploration is technically possible at affordable costs.

Since Eisenhower and Krushchev, political leaders have proposed space exploration as al alternative to confrontation. Mars exploration, when it comes, will be supported by science, education and entertainment industries and hopefully will draw talent from a shrinking armament industry. We cannot at the same time go to Mars and support an arms race.

This year the Institute for Lunar and Planetary Exploration invited a number of Universities to contribute ideas to NASA's baseline Mars Exploration Mission. Such interaction between universities in the U.S. and other nations will compare different approaches, provide broad international understanding and may provide the necessary impetus to the public to make a Mars mission a reality.

Track 5B 1:30

Reducing the Cost of Mars Exploration:

A Summary of Results from the Case for Mars VI, 1996

Tom Meyer,

Boulder Center for Science and Policy

Boulder, CO

The date was July 20th, 1996 - the 20th Anniversary of the Viking Landing on Mars. The occasion was the Case for Mars VI in Boulder Colorado. Conference attendees met for four days to address the challenge of how to inaugurate a program of human exploration of Mars at a reasonable cost and to maintain it at a sustainable level of funding.

Presentations and workshops ranged from discussions of the rationale for human exploration, to innovative technologies and strategies, to management and organizational approaches including international cooperation, to concepts for private sector initiatives.

Against a legacy of rumors dating back to the Bush administration that a return to the moon and a human mission to Mars would cost upwards of $500 billion, a new "faster, better cheaper" challenge emanated from the NASA administration. The goal was to find ways to mount an initial mission to be assembled over an 8-year period for a total cost of $32B (U.S.). Of this, $16B would be the U.S. contribution with an additional $16B being provided by other countries and sources. Such a spending rate would be comparable to that for the Space Station and could potentially be sustained by NASA, though only perhaps after the Space Station was complete. This served as a baseline for deliberations by conference attendees.

A report at the conference on the Reference Mission of the NASA Mars Exploration Study Team went into a detailed technology and mission analysis that included a realistic cost projection that was more than and order of magnitude less than that of Bush era estimates.

Other attendees presented innovative concepts in mission strategy, technology, and management that could yield significant savings. For example, systems for lowering launch costs, dual use of military technology, ideas for low cost structures, and concepts for robotic support were presented. The conference also featured workshops that examined the question of whether there really were any show-stoppers and how to short-circuit needless research. A shopping list of existing technology solutions was developed that covered the gamut of mission requirements from spacecraft and propulsion, to life support, to Mars base infrastructure to show that these did not need to be reinvented. Also addressed was the concept of a non-NASA scenario for a manned mission to Mars.

Track 5B 2:00

International Strategies for the Exploration of Mars

Daryl Hemingway

International Space University

Houston, TX

daryl.r.hemingway1@jsc.nasa.gov

International Strategies for the Exploration of Mars presents the ideas and recommendations formulated by the 1997 Mars Design Project Team at the International Space University (ISU). Its goal is to make a significant and timely contribution to the global effort to explore the planet Mars.

The 1997 ISU Summer Session Program featured a team of 49 professionals and graduate students from 17 countries, who developed a framework of international strategies for robotic and human Mars exploration. The cooperative effort of the multidisciplinary team within a unique, international working environment resulted in the development of strategies that are rooted in current national programs and that will grow beyond the traditional space community to encompass the whole of society.

The outcome of this project is a coherent set of strategies designed to coordinate the numerous activities related to Mars. In addition to the technical program phases of scientific knowledge, resource utilization, and human presence, this report addresses the political, economic, and social aspects. The centerpiece is a strategic roadmap that defines the critical factors, the necessary timelines, and the international framework required for a comprehensive Mars program.

This roadmap assumes three probable main mission goals: to enhance our scientific knowledge, to search for evidence of life, and to undertake human missions to Mars. The analysis of dependent elements, the governing boundaries and the resources needed are examined in order to identify the potential returns of these missions in terms of social, technological and industrial benefits for our societies. Strong international cooperation is envisioned, encompassing a wider number of nations, and even including countries which until now have limited or no significant space activities.

By incorporating the key elements of a successful strategy in each of three possible Mars exploration rationales; planetary science, the search for life and human missions, we have attempted to address decision makers’ immediate concerns in formulating Mars programs. Complementary recommendations for technology development and public support strategies are also provided. The result is not a solution to the Why Mars? question. Instead, International Strategies for the Exploration of Mars is aimed at providing the user with clearly defined requirements and a practical approach that, when implemented, will successfully achieve the desired Mars exploration goal.

Track 5B 2:30

How Could International Cooperation Reinforce the Case for Mars

R. Heidmann

SEP/division of SNECMA

10 Rue Adolphe Vard

27300 - Vernon

France

Rheidmann@aol.com

We need to raise the public interest and make Mars exploration politically desirable. How could International Cooperation help?

When thinking about the future of humankind, people are mainly concerned by global threats: pollution, resources shortage, illnesses, so, a project pushing advancement in related fields of science and technology should naturally be reinforced if globally shared.

People also feel uncomfortable about the growing gap between rich and poor counties; in this sense, a project presented as a means of cooperation is reassuring, and so politically sound.

Technological strength will be more and more viewed as a major factor of competitiveness among nations; know-how improvement and equalization offered by such a program should be perceived by governments as a valuable political opportunity for development and peace.

It is necessary to put Mars exploration in the perspective of mankind spreading out of its endangered birthplace; this can only make sense on a global basis.

How to avoid shortcomings?

Unreliable political commitments: on such a long-term and mediatically fragile enterprise, it is recommended that cooperation be attempted only between politically stable and economically reliable partners, based on a treaty.

Confusing and costly management: to limit overcosts and dilution of decisions, it is necessary to set a centralized international management, politically empowered.

Inefficient industrial organization: development should be in the hands of an international industrial organization based on purely technical and contractual rules (as was done with Ariane).

Can people trust us anymore about costs and schedule? Yes, if we don't oversell the program, really commit industry, and embark on time (based availability of resources and of efficient technologies). Projects should be reviewed by an independent international steering organization.

Last but not least: are we really prepared?

 

Track 5B 3:00

On the Importance and Duty of Colonizing Mars

Josef Oehmen

Landstrasse 81

Titz, Germany 52445

j.oehmen@usa.net

Already nowadays, a great many people are discussing the technical aspects of reaching Mars, and have done so for some 50 years. What becomes quickly obvious is that a sustained human presence on Mars, done that way or this, will certainly place a strong demand on resources and manpower. It becomes thus more and more important to also address non-technical questions of reaching the red planet?

When one encounters for the first time the idea of sending men to Mars and colonizing the red planet, one is instantly absorbed by it: This bold undertaking, this challenge, this impossibility of establishing a continued, and given a little time, largely independent presence of human beings on another celestial body is simply not going to leave one alone. I can hardly imagine any cases where those thoughts, played with a little in one’s mind, aren’t among the most fascinating and exhilarating. The simple thought of leaving Earth and found a new home for mankind among the stars, an outpost of life, is enough to make one addicted to this subject. Then, the whole effort of colonizing Mars seems to completely justify itself beyond the shadow of a doubt. But as deeper as one gets involved with the technical aspects of reaching Mars, the more does it become important to address non-technical questions regarding the establishment of a human presence on one of our neighboring planets.

Fact is: The resources required for the conduct of the research and engineering efforts necessary to establish and maintain a colony on Mars will be considerably. They are, as the subject itself, on a new scale. Fact is that money and manpower and whatever other resource utilized for this purpose cannot be used to support kindergartens or schools, cannot be used to improve the situation of socially disadvantaged and cannot be used to save the poorest of the poor on our planet from starving and the list could go on and on. It will end here, as this should suffice to give a brief glimpse of the responsibility a supporter of the movement to colonize Mars has to accept.

It should be clear that the problem itself isn’t solved by discussing some new fancy ways of working with the industry to get it done without government funding. The question which is to address is the question that has to be answered before any other investigations should be conducted, it is the question of the correctness, it is the question of the legitimization of colonizing Mars.

To state it in expresis verbis:

Is a colonization of Mars worth the necessary money, manpower and resources?

That is the question which will be addressed here and now. As will hopefully be clear in a few minutes, the answer is a clear and untouchable "yes", if we are willingly to accept the responsibilities that come with it. We have to face this truth: If there isn’t some huge payoff of whatever kind inherent to the Mission to Mars, the responsibility of conducting it can hardly be carried.

The solution to this moral and ethical dilemma comes from what at first seems to be the most dangerous threat to a colonization of Mars: Its scale. The sheer dimension of the effort necessary to support an Outpost leaves no choice but to be a true international undertaking.

Mankind has, for the past years, reached a stage of its development where our technical abilities allow us to eradicate all higher forms of life on our home planet within half an hour. But satellite communication, supersonic passenger-airplanes and innumerous other inventions would also allow us to start a planet-wide cooperation, if we choose to do so. The possibilities we have at hand not only make this possible, but they oblige us to use our powers for peaceful purpose, simply because everything else could be fatal.

Never before in the entire history of mankind had we the chance to do anything remotely like crossing the vast of space to colonize another planet. Never before we had the chance to unite all people, regardless of their origin, under one common, peaceful goal. Never before had we the chance to act as a species, not on a timely strictly limited undertaking, but to build our gate to the stars.

With the Mars settlement we have for the first time the truly unique chance to engage in a worldwide, cooperative challenge. It not only requires a planet-wide coordination, it prerequisites the acceptance of the fact that mankind is essentially one, regardless of the place and the circumstances of birth of one of us.

It is our responsibility to spread this thought of Earth and its inhabitants as one planet and one people, it is this what justifies all expenses.

And then, as if there is need for more, there are all the other fascinations and justifications of going into the infinities of space. Just to name a few:

It presents one of the greatest challenges to mankind. Without those challenges, we would enter into a slow, but steady, decline. The function of space programs as turbo-pumps in the stream of technical innovations is obvious.

Secondly, we simply have to leave the Earth sometime. Maybe we could delay this, but sooner or later our home planet will be unable to support any more of us. We can be ready to leave Earth then, or we can pray that everybody prefers birth control to fighting for air, water and food.

And, but now I will become almost unbearably subjective, there are very, very few other fields of human activity where, as is done within astronautics, there is so obviously consciously defined what is possible or not, where there is so openly met the challenge to achieve the impossible, and where there is in such impressive magnitude created reality.

So, what does all this concretely mean, what consequences for our actions does this make necessary? I do have to admit that I am not an expert in politics, but a little common sense should work well in outlining the broad direction:

It has to be expected of the colonization of Mars that it facilitates the installation of one planet-wide agency dealing with our Martian affairs. With this agency, it is our duty to make all possible effort to create an institution which allows mankind over time to grow together, united by common goals and efforts of sustaining and bringing life to the stars, including our home here on Earth. When more and more people realize that it is better for them to place their focus on the destiny of all mankind, the impact in all fields, including the at the beginning mentioned schools and including the poorest of the poor, even the impact in these fields will be immense. Peace and freedom through colonizing Mars. If we choose to do so, than this is our duty.

Mars is not the end of a costly story, Mars is the mark of the beginning of a new era of mankind.

Track 5B 3:30

Space Exploration, Technology Choice, and Social Protest:

Is the Only Way to Get There the Wrong Way?

Victoria P. Friedensen

National Academy of Engineering

2101 Constitution Ave., NW

Washington, DC 20418

Beginning with the premise that the only technologies capable of providing enough power for human transport and support on the surface of Mars are space nuclear power technologies, this paper will analyze the potential problems for a Mars exploration program resulting from social protest of nuclear technologies. Mission planners and spacecraft designers frequently rely on nuclear reactors and radioisotope thermoelectric generators (RTGs) for interplanetary spacecraft propulsion and power supply in transit and on the surface of Mars. Space nuclear power, in the form of RTGs, has a long successful history in the U.S. space program as the most reliable, cost-effective, long-lived power supply for missions outside Earth orbit. Within the current U.S. faster, better, cheaper budget philosophy, nuclear reactors for space propulsion are the most attainable of proposed high-power, long-life propulsion technologies. Frequently, plans and designs for Mars missions assume that these space nuclear power technologies will be cost effective and on the shelf and, with the conclusion that their near-term availability and significant cost savings in advanced technology development, make space nuclear power technologies the enabling technologies for human missions outside Earth orbit. However, recent public protest over the 1997 Cassini mission to Saturn indicates a strong potential for significant social protest over use of space nuclear power that would drive up programmatic costs and risks.

This study will seek to answer whether social protest over, and political dislike of, nuclear technologies will present a significant barrier to the exploration and eventual colonization of Mars. The potential problems will be outlined and potential solutions offered.

Track 5B 4:00

One Way to Mars/a Permanent Settlement on the First Mission

Bruce Mackenzie

Boston, MA

BMackenzie@draper.com

 

One way to set up permanent settlements on Mars is to plan one-way trips instead of round trips.

It may be less expensive and safer to set up a permanent base on the first human missions to Mars, than to have round-trip missions. Of course, there must be some way for the people to return, if required. But, if the people plan to stay, we might save enough on their return flights to send the extra equipment and tools to set up a permanent base immediately.

Advantages of One-Way to Mars:

  1. The most hazardous part of the Mars mission may be the return flight.
  2. It is more expensive to transport people back form Mars than to Mars.
  3. The major reason to go to Mars is for permanent human settlements.
  4. Scientific investigations, the second reason, would be much easier with a permanent Mars settlement.
  5. Robotic instruments can gather information needed to design equipment and plan settlements, which was not possible for pioneers historically.
  6. "Opening a New World" is a stronger motivation than the "Flags and Footprints" method of Apollo.

Track 5B 4:30

International Collaboration as a Path to Mars & Beyond

Developing an International, Operational Space Organization

Dave Kisor

1616 Crown St.

Clearwater, FL 33755-2811

geocat@hotmail.com

While just over twenty nations either possess their own space agency or are members of a consortium, over two hundred nations, many of which are considered "developing", are potential members in this "exclusive club". Many of these nations are just struggling to survive and some have no true central government due to civil war and other such catastrophic societal events and would otherwise find it unthinkable to send anyone into space. Any of these nations interested in joining the space fairing world could be introduced to a technology slightly higher than their general public is presently accustomed to and brought up to speed.

This would be more of a "bootstrap" in the beginning, as everybody must begin somewhere and should not conflict with the United Nations' Space Organization. The UNSO, like most UN organizations, is designed to oversee treaties and perform related functions, not to oversee spacecraft development, mission planning and other functions required to depart a planetary body. However, many of the nations actively engaged in space research are members of the UNSO. Business and academe from space faring nations would start the training and eventually hand operations over to those whom they have trained as part of a noncompetitive, cooperative agreement.

Providing the potential for a truly international space organization requires participation from the majority of nations, not simply the few nations already engaged in space flight

Track 5B 5:00

Design Projects at UC Berkeley for NASA's Heds-Up Program

Larry Kuznetz

University of California at Berkeley

Berkeley, CA

n2mars@aol.com

Missions to Mars have been a topic for study since the advent of the space age. Because of financial and political constraints however, human missions have been relegated to backroom efforts such as the Space Exploration Initiative (SEI) with it's 90-day study in 1989-90. What funding exists has largely been reserved for the unmanned probes such as the Viking landers, Pathfinders and Global Surveyers. With the newfound enthusiasm from Pathfinder and the meteorite ALH84001, however, there is renewed interest in human exploration of Mars. This is manifest in the new Human Exploration and Development of Space (HEDS) program that NASA has recently initiated. This program, through its University Projects (HEDS-UP) office has taken the unusual step of soliciting creative solutions from universities.

Design Projects:

For its part in the HEDS-UP program, the University of California, Berkeley was asked to study the issues of Habitat design, Space Suits for Mars, Environmental Control and Life Support Systems, Countermeasures to Hypogravity and Crew Size/Mix. These topics, as well as the interactive design environment (IDE) have been design projects in "Mars by 2012", an ongoing class for undergraduates and graduate students. The IDE is an electronic resource that allows NASA scientists and engineers, as well as the public, to interact with and critique engineering designs as they progress. It usually takes the form of a website (in this case, http://mars2012.berkeley.edu) that creates a "virtual office" environment whereby NASA and others can interact in a constructive manner to propose and review concepts or relationships for potential inclusion in NASA's Mars Design Reference Mission. For the Mars Forum, we will present the basics of the IDE insofar as it relates to the HEDS-UP program, and a proposal for a flight experiment to determine the need for artificial gravity on human Mars missions, based on the results of our design project studies.

7:00 Plenary Panel B

The Preservation of Extraterrestrial Life

Mark Lupisella
NASA/Goddard Space Flight Center
Greenbelt Rd.
Greenbelt, MD  20770
Mark.Lupisella@gsfc.nasa.gov

As we expand our presence in the solar system and beyond, novel and challenging scientific and policy issues will face us.  A relatively near-term issue requiring attention involves questions regarding the search for and discovery of primitive extraterrestrial life-Mars being an obvious
candidate.  Such a search and potential discovery is clearly of paramount importance for science and will pose novel and challenging mission planning and policy questions regarding how we should search for and interact with that life.  This paper will explore the scientific and mission planning issues along with the policy issues associated with the search and interaction with primitive extraterrestrial life.

Central to the logistical science and mission planning issues is the role and feasibility of modeling techniques.  Central to the policy questions are issues of value. Exploring this overall issue responsibly requires a holistic understanding of how both of these aspects of the issue interrelate.

Some of the questions to be considered are: Will contamination jeopardize or mask possible indigenous life forms? To what extent can we control contamination (e.g. will it be local or global?) What are the criteria for determining the biological status of an extraterrestrial planet like Mars
(e.g. for example, can we extrapolate from a few strategic missions?) What will our policies be regarding our interaction with non-intelligent extraterrestrial life?

7:00 Plenary Panel B

Otherland Ethics

George Smith

23 Lexington Ave. No. 1739

New York, NY 10010

GeoSmith@msn.com

A serious and durable Mars exploration effort-one capable of garnering widespread respect and support needs an intelligible and systematic framework for approaching issues of environmental ethics. This presentation proposes a practical ethical system developed by an unaligned professional, and shows how it works when applied to a particular problem (terraforming).

The first part of the presentation will briefly describe the interconnectedness of space exploration and environmentalism, then move to a critical analysis of contemporary approaches to environmental ethics. Special focuses: the notion of ethical extension; the problem of demarcation; the proliferation of centrisms (anthropocentrism, geocentrism, biocentrism, cosmocentrism, etc.); the preference for general theories of value rather than practical ethical systems; the call for a cosmocentric ethic; the neglected polycentricity of practical ethical systems.

The second part of the presentation will set out the main features of a mainstream, philosophically-justified ethical system that can be characterized as: (a) rule-based, in that it centers on a specific set of general moral rules; (b) rationalistic, in that it does not depend upon concepts that are unanalyzable or transcendent; (c) sentience-oriented, in that it makes the demarcation decision in terms of sentience or consciousness; and (d) empirical, in that it depends upon a balancing of predictable harms and benefits, and tends to push ethical inquiry in the direction of measurable facts.

The third part of the presentation will be an application of the proposed system to a particular scenario: Assume humans have extensively explored and studied Mars, including indigenous microbes found in vents a mile beneath the surface. The outpost has evolved into a permanent colony, and the colonists have developed plans for a long-term terraforming project. Should the plans proceed?

The presentation will conclude with a brief evaluation of the proposed system, from both space-exploration and environmentalist perspectives.

7:00 Plenary Panel B

Ethical Considerations in Planetary Engineering

Chris McKay

NASA Ames Research Center

Moffett Field, CA

 

The Duty to Terraform

Robert Zubrin

Pioneer Astronautics

445 Union Blvd. #125

Lakewood, CO 80228

Terraforming a Cradle for Life

Prof. Greg Benford

University of California, Irvine

 

TERRAFORMING THE PLANETS: Mars

Lowell Wood

Hoover Institution, Stanford University

Stanford CA 94305-6010

Mars presents the most obvious example of potential human capabilities for transforming the surface conditions of other Solar planets into ones suitable for support of technically unaided human life, primarily due to its current congeniality to lightly-aided human activities on and near its surface, i.e., to the comparatively modest distance in parameter space which must be traversed to attain Terra-like conditions.

Two basic scenarios for terraforming Mars are discussed, In the more optimistic one, a one-time heat-pulse suffices to convert present Martian near-surface conditions into ones which then may be readily engineered into ones acceptable for unaided human activities, bootstrapping into existence an atmospheric heat-trap of sufficient magnitude and exploiting the materials presently trapped in the Martian polar caps and positioned within a few meters of the Martian surface. The more pessimistic one assumes that a significantly larger steady-state heat input, relative to present conditions, will be required to maintain terrestrial-like conditions. Independent sets of ways-and-means of engineering within either of these scenarios are presented, supported with first-level details. Due to the planetary scale, solar insolation is the only feasible heat-source, and effective insolation modulation – either through increasing the Martian optical cross-section or by varying the planet's (time- and frequency-dependent) albedo – is the common feature of all such schemes.

The essence of practicality lies in the minimization of mass and energy required to accomplish the necessary insolation modulation. The most elegant approaches exploit latent instabilities in the Martian climatological system to increment surface temperature by several dozen kelvins with asymptotically small albeit exceedingly potent human interventions.

Notably, it appears feasible to fully terraform Mars on a three-decade time-scale – to create and operate an actual ''Genesis Machine'' within a single gigasecond – a duration well within the lifetimes of the first Mars-men, moreover while employing resource levels denominated in millionths of the current U.S. GNP.

 

Saturday Plenary Session 9:00

Life on Mars: Past Present and Future

Chris McKay

NASA Ames Research Center

Moffett Field, CA

Mars was once a warm and wet planet, a place friendly to life. It could potentially be made so again. By exploring Mars, we may be able to resolve the question of whether the origin of life involved processes that were unique to the Earth or common in the universe. By settling Mars, and attempting to terraform it, we may answer the question of whether life is capable of spreading from its planet of origin.

Saturday Plenary Session 10:00

Mars for Profit

Jim Benson

SpaceDev

San Diego, CA

 

It should be possible to conduct robotic Mars exploration on a for-profit basis. The author is the founder and CEO of SpaceDev, a private corporation dedicated to space exploration for profit. SpaceDev is already raising funds for a near-Earth asteroid mission, and is interested in the possibility of undertaking Mars missions as well.

Saturday Plenary Session 10:30

Roles for Free Enterprise and Government in Opening the Space Frontier

Rick Tumlinson

Space Frontier Foundation

Los Angeles, CA

Saturday Plenary Session 11:00

Going to Mars: An Astronaut’s Perspective

Lt. Col Scott Horowitz

NASA Johnson Space Center

Houston, TX

The author, a professional astronaut, will give his views on the human Mars mission, including such issues as our current technological readiness, medical concerns, mission risk, and desired crew composition.

Saturday Plenary Session 11:30

The Use of Robotic Precursors to Open the Way to Human Mars Exploration

John Connolly

NASA Johnson Space Center

Houston, TX

NASA’s current robotic Mars exploration program can and should be used as a means of demonstrating key technologies and resolving environmental unknowns to prepare the way for human Mars exploration.

Brown Bag Lunch Event 12:00

SSTO, Pathway to Mars?

Bruce Lusignan

Center for International Cooperation in Space

Stanford University

Stanford University has completed the third iteration design of a Single Step to Orbit Launch system to replace NASA's Shuttle.

The aerospace industry is aware that the true Singe-Stage-to-Orbit vehicles, whether Vertical or Horizontal take-off, or Vertical or Horizontal landing, do not get useful payload to orbit, despite large research monies spent on studies and tests. What does work is a rocket planet that starts out fully fueled at 40,000 fee and has wings to assist in the flight from there to orbit. The rocket equations show you can get a useful payload (9 Metric Tons) to Low Earth Orbit or (25 Metric Tons) to Low Earth Orbit with an apogee kick stage. Three configurations of such single Step to Orbit space planes are feasible. One is Kelly Enterprise's, where the fully fueled rocket plane is towed to altitude by a tow plane. One is suggested in a Hotl proposal, where the fueled space plane is flung from the back (or dropped from the belly) of a carrier plane. A third follows Mitch Clapp's Black Horse concept, where the rocket plane takes off with jet engines and payload, then meets a tanker plane to load on the liquid hydrogen and then flies on to orbit.

The air-fueling configuration offers significant advantages in development and testing and more viable abort scenarios. The Stanford SsTO is based on the air-fueling concept using the largest Antonov cargo plane to carry the liquid oxygen.

The SsTO can deliver 15 metric tons to Low Earth Orbit using a parabolic flight and apogee circularizing motor. The circularizing motor remains with the fuel forming a "space tug" that can be used to support deep space exploration. The tug costs about $25 million including the hardware and SsTO launch.

The design of Mars Direct by Bob Zubrin, the Base Line study by NASA's Johnson Space flight Center, and the Stanford-Russian Human Mars mission use a number of cargo flights to Mars followed by the exploration crew. Less than 40 space tug modules at a total cost under $1 billion, would propel the five to seven mars vehicles needed for these missions. The Mars Missions should be reviewed based on the availability of such low cost in orbit fuel modules. We support the suggestions that NASA stimulate a private international consortium to develop a SsTO by committing to purchase fuel modules in orbit to support human Mars missions.

Brown Bag Lunch Event 12:00

Boosters for Manned Missions to Mars, Past and Present

Scott Lowther

Pioneer Astronautics

445 Union Blvd. #125

Lakewood, CO 80228

A large number of space launch boosters have been proposed throughout the years, many of which were designed for or were applicable to launching components required for manned missions to Mars. In this paper, past and current designs for booster vehicles needed to perform manned Mars missions are examined and compared, with emphasis on current and very recent concepts. Included are such designs as: von Braun’s 1952 Ferry Rocket, the Saturn V and various Saturn V derived vehicles, various Nova studies from the 1960’s, the Soviet N-1, the Soviet Energia, various Shuttle Derived Vehicles (such as Shuttle-C, Aries and similar designs) , the Evolved Expendable Launch Vehicle, VentureStar, StarBooster 400, StarBooster 1800 and Magnum. Vehicle designs are described and shown and capabilities are compared, along with any manned Mars mission modes originally proposed for each booster. The utility of each booster for Mars piloted and cargo missions at current technological levels are examined.

Three baseline Mars missions based on modern technology are also to be briefly described: A Mars Direct architecture, the current NASA-JSC Design Reference Mission architecture and a stereotypical large on-orbit assembled single vehicle. These missions are then modified for each booster, showing the modifications required, if any, to the mission in order to utilize a certain launch system. The results are then compared and contrasted. Conclusions are drawn based upon these results, with certain boosters showing a higher level of ability and confidence.

Brown Bag Lunch Event 12:00

Next Generation Launchers in the Exploration of Mars.

Gary McPeters

The exploration of Mars has been conducted exclusively by governments using launch vehicles developed by government. In the future, this exploration may be conducted by private groups using launch vehicles developed by private industry. This new generation of launches is being developed by familiar names like Lockheed-Martin and newcomers like Kistler Aerospace, Pioneer Rocket Plane, and Rotary Rocket. These vehicles will be horizontally and vertically landed, manned, unmanned rockets and jet powered, single and multi-staged. But they will share the attributes of increased launch rates, quick turnarounds and lower costs. These characteristics will change the way we explore Mars. Cheaper launch costs mean private groups will be able to launch probes to Mars. Money saved on launches can instead be spent on payloads. More launches offered by more companies mean more payloads can be sent in every launch window to Mars. Instead of one or two probes, we could get fleets.

Further ahead, the advent of manned launchers and single stage to orbit vehicles will rapidly open the possibilities of large scale Mars exploration. Single stage to orbit launchers will offer the most exciting uses when they become operational. If they are refueled in orbit, their Delta-V capacity will enable them to take their payloads directly to Mars. Since they are designed to use aero-braking to land on Earth, they will be able to use it at Mars, increasing their payload capacity even more. These reliable, operational vehicles could then become a new class of Mars

transports without costly design of new vehicles.

This and more will be made possible by the new generation of launch vehicles.

Track 1C 1:00

Oxygen Generation on Mars Using Solid Oxide Electrolysis

K. R. Sridhar,Space Technologies LaboratoryThe University of Arizona

Tucson, Arizona

krsridhar@mail.arc.nasa.gov

Generation of oxygen on Mars for life support and propulsion needs will have a significant impact on reducing the cost and launch mass of human missions to Mars as well as robotic sample return missions. This talk will address the solid oxide electrolysis technique for generating oxygen from carbon dioxide. In this solid state process, carbon dioxide is decomposed to carbon monoxide and oxygen, and the oxygen thus produced is separated electrochemically by a nonporous ceramic

electrolyte. Laboratory level demonstrations have shown that the process is robust, and will operate in Mars simulant atmosphere for extended periods (tested for over six months) with no noticeable

degradation in performance. The principle of operation, mass and energy needs and its potential role in Mars exploration will be discussed.

A proof-of-concept electrolyzer will fly on the 2001 Lander to Mars. An integrated Mars Oxygen Generator System (OGS) concept which is part of the Mars ISPP Precursor (MIP) flight experiment is presented. The electrolyzer is based on a planar zirconia disk configuration. The proposed packaging of the electrolyzer within a 100 mm diameter and 100 mm high cylindrical container limits heat losses to less than 10W. The complete OGS includes flow control and sensing hardware. The design details of the payload will be presented. This will be the first payload ever to generate resources of use to humans from planetary materials

Track 1C 1:30

Production of Higher Hydrocarbon Species on Mars

Brian M. Frankie, P.E.

Dr. Anthony C. Muscatello

Pioneer Astronautics

445 Union Blvd. #125

Lakewood, CO 80228

 

While in situ propellant production (ISPP) is widely recognized as one of the key technologies required for the exploration and eventual settlement of Mars, most ISPP concepts are troubled by the "hydrogen question." The majority of ISPP concepts require some form of hydrogen feedstock to the process, as hydrogen is required in most liquid fuels, but is not easily available on Mars. Hydrogen transport as water, ammonia, or methane is possible but limits the mass leverage of the ISPP system, so most concepts have proposed transporting liquid hydrogen to Mars. Liquid hydrogen is a low density extreme cryogen, and has an annoying tendency to leak, which increases the difficulty of transport. This paper examines options for producing liquid fuels that have low hydrogen content, which both helps alleviate the difficulties of hydrogen transport, and increases the mass leverage of the ISPP system. In addition, as the human presence on Mars expands beyond the initial exploration phase, low hydrogen content compounds will have additional uses as chemical feedstocks. The low hydrogen content fuels of primary interest, in order of interest, are aromatics, olefins, and high molecular weight paraffins.

Track 1C 2:00

Prospects for the Utilization of CO2/Metal Propulsion on Mars Ascent Vehicles

Evgeny ShafirovichInstitute of Structural Macrokinetics,Russian Academy of Sciences

Chernogolovka 142432, Russia

The present paper deals with the concept of a rocket using Martian carbon dioxide as an oxidizer and metals or their hydrides as fuel. Calculated performance characteristics of the rocket and the known data on ignition and combustion of metals in CO2 are analyzed. It has been shown that beryllium hydride ensures the highest specific impulse. However, the lack of information on combustion of metal hydrides in CO2 and, on the other hand, the fairly good ignition and combustion characteristics for magnesium with CO2 allow the conclusion that currently only magnesium fuel can be considered as fitting for rocket engines using CO2. Possible design types of the CO2/metal rocket engine are considered. Hopper and sample return missions with visiting several sites on Mars surface are analyzed. It has been shown that such missions become advantageous if the CO2/metal engine is used. The use of Martian CO2 as an oxidizer in rockets appears as an attractive way to long range mobility on Mars. The hopper mission using CO2/metal propulsion might be considered as a next significant leap forward compared to the performed Viking and Pathfinder missions. Results of recent experimental studies on ignition and combustion of single levitated particles of Mg and Mg-Al alloy in carbon dioxide [1] are discussed from the standpoint of Mars propulsion applications.

REFERENCE[1] Legrand, B., Shafirovich, E., Marion, M., Chauveau, C., and Gökalp, I., "Ignition and combustion of levitated magnesium particles in carbon dioxide," 27th International Symposium on Combustion, August 2-7, 1998, Boulder, CO, The Combustion Institute, Pittsburgh, in press.

Track 1C 2:30

Oxygen Extraction from Martian Atmosphere using Radio Frequency Discharges

R.L. Ash, T. Dinh, S. Popovic, and L. Vuskovic

Old Dominion University

Norfolk, VA 23529

Studies starting in the late seventies have shown that Mars' atmosphere can be use as a feedstock for oxygen production using simple chemical processing systems during early phases of the Mars exploration program. This approach has been recognized as one of the most important in-situ resource utilization (ISRU) concepts for enabling future round trip Mars missions. We have been working on the development of capacitive and inductive radio frequency (RF) discharges for oxygen production. The capacitive RF discharges increased the conversion efficiency of carbon dioxide into carbon monoxide and oxygen at lower temperatures and were combined with oxygen separation using a silver membrane, which acted as one of the electrodes in the discharges. The discharges were operated at pressures typical for Martian atmospheric conditions. Mars atmospheric simulant gas was used, which contained practically exact proportions of carbon dioxide, nitrogen and argon as in the actual Martian atmosphere. The results of computer modeling, confirmed by experiment, show that the chemical composition of Martian atmospheric gas is changed in the RF discharge. The Mars simulant gas was transformed into the mixture containing large proportions of atomic and molecular oxygen, carbon monoxide, and proportionally smaller amounts of carbon dioxide and other gases. The residual gas, after partial separation of oxygen, has a potential for further utilization as a "dirty" carbon monoxide fuel. The property of the RF discharge to trap and enable natural removal of dust particles is also recognized and elaborated. The systems based on RF discharges will be compared with other ISRU oxygen extraction methods with respect to size, mass, power, efficiency and oxygen quality.

 

Track 1C 3:00

Current Progress in Water Reclamation Technology

Dr. Bradley S. Tice

Director and Institute Professor of Chemistry

Advanced Human Design

P.O. Box 2214

Cupertino, CA 95015-2214

The presentation is a review of the current status on research conducted at Ames-NASA Research Center in the area of water reclamation technologies. Details in the following areas of research will be explored.

  1. Advanced Oxidant Delivery Screening
  2. Catalyst Screening
  3. Development of Special Catalysts

An overview of future research as applied to human habitation of Mars and the Moon will conclude this session.

Track 1C 3:30

Site Selection on Mars Based on Optimal Collocation of Indigenous Resources

Donald Barker, M.S., M.A.

George James, Ph.D.

Gregory Chamitoff, Ph.D.

gregory.e.chamitoff1@jsc.nasa.gov

Like the Earth, Mars is a planet with an abundance of natural resources, including accessible materials that can be used to support human life and to sustain a self sufficient Martian outpost. Major in situ resources required by the initial inhabitants and explorers include water, atmospheric and material consumables, and various energy and fuel reservoirs. This paper examines the potential for supporting the first manned mission with the objective of economically achieving self-sufficiency through well understood resource exploration and identification, followed by a program of rigorous scientific research aimed at extending and expanding in situ resource utilization capabilities. The potential for initially extracting critical resources from the Martian environment is examined, and the scientific investigations required to identify additional resources in the atmosphere, on the surface, and within the subsurface are discussed. The current state of knowledge regarding the planet's geomorphology is examined, particularly as it pertains to the question of locating water and other useful resources. Questions of scientific necessity and feasibility are examined with respect to the concepts of resource utilization and habitability. Throughout the next decade, unmanned precursor missions, including Pathfinder, Mars Global Surveyor, and the Mars 98, 2001, 2003 and 2005 missions, can and should be targeted and utilized to construct an initial resource knowledge database that will serve to support the selection of an initial manned landing site. Considerations are presented for determining the optimal landing site based on the best combination of the known and potential existence and accessibility of Martian resources. The primary goal of achieving self-sufficiency on Mars would accelerate the development of Human colonization beyond Earth, while providing a robust and permanent Martian base from which humans could explore and conduct long term research on the evolution of planets, the solar system, and life itself.

 

Track 1C 4:00

Phobos on the CheapGeorge William HerbertRetro Aerospace

gherbert@crl.com

Prior manned Mars exploration architectures have proposed, with good reason, that manned exploration proceed directly to the surface of Mars once we begin sending humans to the Mars system. Phobos on the Cheap proposes instead that we take a slow approach, incrementally building up towards an eventual manned landing. First, the propulsion area is addressed by providing a reusable low thrust deep-space propulsive ion drive tug disguised as a commercial transfer stage product for LEO to GEO missions. Once that vehicle has been flown and demonstrated, it begins being used for unmanned Mars missions, as it reduces the cost of delivering payloads to Mars substantially. When the tug has been proven in deep space applications, we expand the program to create a manned base on Phobos, suitable for long term habitation and tele-operation of Mars surface rovers, giving many of the benefits of humans on the surface with few of the costs. Finally, after the Phobos base operation has been built up and extensive robotic and tele-operated surveys have been completed, we develop a surface landing program sending humans to explore the most interesting sites identified in the tele-operated science program. Each of the steps independently is a low risk, low cost step, but together they march towards an ongoing, sustainable, and affordable manned Mars exploration campaign.

Track 1C 4:30

Polar Options for a First Mars Expedition

Geoffrey Landis

Ohio Aerospace Institute

NASA Lewis Research Center

21000 Brookpark Rd.

Cleveland, OH 44135

A first Mars expedition will be greatly facilitated by use of in-situ Mars resources for producing return propellant. While most discussions of Mars resource availability assume that a Mars mission will target an equatorial or mid-latitude site, I argue here that there are significant advantages to a polar site. Polar regions have two distinct advantages over lower latitude sites.

Polar regions facilitate easy access to mars volatiles in the form of frozen water and carbon dioxide. This is important not only for production of rocket fuel for the return to Earth, but for production of fuel for local mobility. A polar expedition would not have to bring hydrogen from Earth to produce propellant, but could extract hydrogen by simply melting available ice.

Also, during the Mars summer, both the Sun and the Earth are constantly above the horizon. This allows continuous power generation without the requirement for heavy power storage systems, and allows direct communications to Earth.

While a polar site may be less desirable for geology, since the terrain is ice-covered, geological studies of non-ice-covered terrain can easily be accomplished by use of a long-range rover, and there are unique exploration possibilities to gather information available from polar science which are not found elsewhere on the planet.

Track 2C 1:00

Martian Law: The Case for A Global Democracy

Thomas Quinn

Evolutionary Theory Outreach Group

P.O. Box 510373

New Berlin, WI 53151

Homo sapiens will soon enter into a new era when we colonize Mars and become a multi-planet species. This event will trigger some tough legal questions, but perhaps none will be as difficult as who should rule Mars. Although many possibilities exist, there are some solutions that appear to be better than others. A detailed comparison of the possible options will be presented within the historical context of past colonization events on Earth and their outcomes. The analysis suggests that the best solutions for the future inhabitants of Mars would be the following:

. Martian citizenship should be freely granted to all colonists on Mars.

. A single, global democracy for the entire planet should be established.

. Local decision should be decided by the individual colonies.

The simple precept that "Martians should rule Mars" would likely prevent potential problematic outcomes, like war or serfdom, from occurring. Mars should be a politically independent entity; however, this autonomy will be somewhat limited as it seems that Martians would remain economically dependant on Earth for many supplies, materials, and resources. Until permanent colonies can be established on Mars, a "hands-off" policy is the most just thing to do. I present a prototype for a Mars treaty, based on The Antarctic Treaty of 1959, for future discussion on the topic. Using Antarctica as a model, this treaty would be designed to keep Mars in the public domain for research and exploration while protecting the planet from the tragedy of the commons.

Track 2C 1:30

Martian Law

Dr. Edward L. Hudgins

CATO Institute

Washington DC

ehudgins@cato.org

A country's economic development and utilization of its resources depend foremost on the country's economic, legal and political regimes. The fall of communism and state-directed systems in poorer countries seem to herald the victory of the free market. That regime gives maximum incentives for individuals to utilize the ultimate source of values, the human mind, to create wealth. But misunderstandings about markets have led to rough transitions.

The model for Mars is not the Antarctic Treaty nor the Law of the Sea Treaty. These versions of the statist regimes now rejected by most countries would ensure that Martian resources remain unexploited. In fact, flawed elements of the Outer Space Treaty and the Intelsat Agreement already have slowed the private sector space development.

Mars will need an economic/legal regime based on property rights and contacts. Initial planetary development will depend on consortia arrangements that serve immediate needs. But consortia must allow for a transition to a system with market prices, the only efficient way to allocate resources, and with incentives for entrepreneurial innovation.

Public health and safety functions, currently provided very poorly by governments on Earth, might be guaranteed more efficiently by incorporating their goals into initial consortia rules and contracts. The extensive research and insights market thinkers in past three decades can help Mars avoid the mistakes that all Earth governments now are trying to correct.

Attempts by merchants in the Age of Exploration 500 years ago profit though trade in a world without law gave rise to innovative market institutions like double-entry bookkeeping and insurance (a means to share risk). The development of Mars, if done right, will not only be yield advances in science and technology, but in free, civil institutions as well.

Track 2C 2:00

Red, White and Blue Mars: The Case For American Ownership

Alex Lightman

1431 Ocean Ave., #419

Santa Monica, CA 90401

alex@hollyworlds.com

Who owns Mars? Currently, no one does, or everyone, depending on how one interprets two different UN Treaties. The natural consequence of this is that Mars will remain untouched by human hands, or feet, for the foreseeable future, since the cost of a manned mission will be comparable to the largest projects in history. As Americans and others around the world view the latest images beamed back to earth from Mars Surveyor, now is the time to ask whether all we want from the red planet are pictures.

The United States should claim Mars in the near future, or ask to become a trustee for Mars until it can be self-governing. In weighing the advantages, disadvantages, justifications and probable consequences, we may find that there are few actions that could be taken by the United States with such profoundly beneficial consequences. America could increase its wealth, power, influence, security, and confidence in the future. The cost would be virtually insignificant, a rounding error in our $1.7 trillion federal budget. With an aggregate stock market value of over $15 trillion, and a national valuation of almost $70 trillion, development of Mars is well within America's capabilities. The catalyst will likely be property rights, the same catalyst for the rapid rise of both Europe and the United States compared to their contemporaries in the middle ages and over the last two centuries.

What are the obstacles? Basically, one article in the first UN space treaty, and two in the second. Though the US ratified the first treaty, it has not ratified the second, and neither have over 170 other nations.

1. Article II of the "Treaty on Principles Governing the Activities of States in the Exploration and Use of Outer Space, Including the Moon and Other Celestial Bodies" that entered into force in 1967 states:

"Outer space, including the moon and other celestial bodies, is not subject to national appropriation by claim of sovereignty, by means of use or occupation, or by any other means."

2. Article XI of the "Agreement Governing the Activities of States on the Moon and Other Celestial Bodies" (1979) states, in section 2:

"The moon is not subject to national appropriation by any claim of sovereignty, by means of use or occupation, or by any other means."

3. Section 3 goes further: "Neither the surface of the moon, nor any part thereof or natural resources in place, shall become the property of any State, international intergovernmental or non-governmental organization, national organization or non-governmental entity or of any natural person. The placement of personnel, space vehicles, equipment, facilities, stations and installations on or below the surface of the moon, including structures connected with its surface or subsurface, shall not create a right of ownership over the surface or the subsurface of the moon or any areas thereof. The foregoing provisions are without prejudice to the international regime referred to in paragraph 5 of this article."

These two paragraphs are the only 'obstacles' to America's claim of sovereignty. Comparing these agreements to the benefits that will accrue to 265 million Americans, and eventually to the other 5 billion or residents of this planet, we may come to the conclusion that the US government should either ignore these provisions, or give the one year notice that we are withdrawing from the 1967 treaty (the only one we have ratified) which the treaty offers any signatories. Just say "no" to pointless UN limitations. Pass a law permitting Americans to file claims to land and other resources of Mars, via the Patent Office unless a specialized agency is set up.

The case for American ownership of Mars consists in part of approximately 24 reasons, including several of the following:

Why not claim Mars for the United States? If Mars were an American possession, the images that we can download from the Internet would take on new meaning. We might imagine that we are looking at a future state, a place to visit, develop mining and other new businesses, and develop the next phase of human civilization.

Track 2C 2:30

Legislation and Space Law Concepts Proposed for the Eventual Industrialization of Mars by Man

James J. Hurtak, Ph.D.

AFFS Corporation

jjh@affs.org

Mars offers the opportunity for the US and world powers to establish significant cooperation in exo-industrialization and exo-commercialization. A new set of 'Space Law' requirements is proposed for human settlement, scientific discovery, and industrial explorations as a result of strategic overlays of international cooperation and evolutionary growth of bottom-up technical validation of conditions favorable for international Martian exploration. A closer evaluation of needed laws clarifying "sovereign territory" versus the "common heritage of mankind" is examined according to international and politically determined agendas supported by technical trade studies so as to avoid confusing and wasteful uses of planetary resources and technology that may cross the boundaries of national logic and security.

Here an approach is applied to the task of developing a robust set of comprehensive legal requirements for the major system elements and mission scenarios necessary for utilizing potential energy and mineral resources. Commercial activities in outer space will function in a way similar to that of the Law of the Seas, where the resources in outer space are open to all. The Law of the Seas has often been stated as the guidelines of international space law. Space must begin to be defined as either res communis or res commercium as interplanetary activity increases in the 21st Century. In usage of the former form, we would envision the possibility of international ownership of satellites, exploration and development through an international regime or a Cosmic Development Corporation (CODEC).

References:

[1] Basic documents of International Law, 3rd Edition. Ian Brownlie, Ed., Oxford University Press, 1985, p. 205.

[2] Convention on the Law of the Sea (Part I-XVII) United Nations Records, April 30, 1982.

[3] J.J. Hurtak, Extraterrestrial Imperative and the New Image of Man in Space, paper delivered at the United Nations, October 1996.

Track 2C 3:00

Legal Implications of the Moon Treaty Relative to the Exploration and Settlement of Outer Space

Elliot D Yug

Attorney & Counselor at Law

333 S. Third Street, Las Vegas, NV 89101

We live in exciting times with regards to space law in general and the "Moon Treaty" of 1972, particular. The "Moon Treaty" introduced the concept of the Common Heritage of Mankind to outer space. Under the "Moon Treaty" any exploitation of extra-terrestrial natural resources must be done under the auspices of the United Nations.

There are two proposed projects on the drawing boards which may well run afoul of the "Moon Treaty". NEAP is a private project which proposes to return samples from a near Earth asteroid for scientific research.

In his book The Case for Mars, Robert Zubrin proposes a plan for the exploration and colonization of Mars. Under this plan, explorers will "live off the land" and a colony will eventually be self-supporting by means exploiting Martian natural resources.

Both projects raise several questions:

  1. Give the fact that the United States has never signed the "Moon Treaty" are its nationals subject to the treaty.
  2. Assuming that U.S. nationals are subject to the treaty, does the treaty preclude all exploitation or just for-profit exploitation;
  3. At what point in the development of a Martian colony does non-profit exploitation during the exploration of Mars become for-profit exploitation as Martian natural resources are used to support the colony itself; and,
  4. Are the restrictions of the "Moon Treaty" applicable to a Martian colony as it becomes self-supporting?

Track 2C 3:30

Mars Governance

Declan O'Donnell

President, World Space Bar Association

3300 East 14th Avenue, Denver, CO 80206

In order to assist the persons who are settling Mars, there are several concerns that should be resolved in advance in respect to Mars Governance. The threshold level of concerns relates to standards, planning, legal tender, municipal services and the concept of authority in the community. It is asserted that Mars Governance has unique and specific needs, ones that will dovetail with the kinds of missions to be developed or promoted by the Mars society. These will be reviewed and catalogued. Mars Governance is thereby different from, and independent from, space governance paradigms generally, albeit a future reconciliation is possible, if and when such is ever developed. The assertion includes the proposition, therefore, that Mars Governance has priority. It also suggests that the Mars Society should take a leadership role in that process. The paper will suggest how to proceed on these assumptions.

Track 2C 4:00

The Rights of Mars

Robert Zubrin

Pioneer Astronautics

445 Union Blvd. #125

Lakewood, CO 80228

In the past, new lands have served as laboratories for "noble experiments" in which new sets of rights could be tested as means of organizing human society on a more progressive basis than deemed practical in well-settled and organized home countries. The most obvious example of this process is the United States, in which a collection of basic rights, including freedom of press, religion, assembly, trial by jury, right to bear arms, and to vote for representative government were implemented in the face of widespread skepticism of educated European opinion, and by their success, set the pattern for the reorganization of human society on a higher basis globally. The author believes that there is a need for this process of experimentation to continue, and that Mars could serve as the laboratory for a further set of noble experiments, that could help humanity find its way to a still more human form of society

Track 2C 4:30

Good Fence Makers

Rick Alan

127 Top O’ The Lake Drive

Lakeway, TX 78734

r.alan@ieee.org

 

He only says, "Good fences make good neighbors."

This is a line from a poem by Robert Frost which derided fences as unnecessary and the sign of a closed, petty mind. He was wrong. Good fences are the enshrinement of property rights in law. Good fences make good boundaries and good boundaries define freedom, a prerequisite to brotherhood. Good fences do not make good neighbors; good neighbors make good neighbors, but good fences can help us get along.

Good fences are symbolic of the value of every human being as a human being. Being human means making moral choices, which presupposes freedom. Slaves cannot be good or bad since they can't choose their acts. Slaves have no fences.

Much of what has gone wrong with America can be viewed as the loss of good fence making ability, usually in the name of some variant of "caring" or "compassion". My thesis is that caring and compassion lead to fences, not away from them.

Mars is humanity's chance to try again to establish a commonwealth of liberty, a practical brotherhood where rights are limited and sacred. America was once the "last, best hope" of humanity: but that isn't said much anymore. Let's say it about Mars.

Let's say it about Mars before we lose it to some misguided attempt to declare it out-of-bounds to humanity, life Antarctica. Let's fence it in before we're fenced out.

Let us build fences on Mars, if at first only in our hearts here on Earth. Let us make both beautiful. Let us be good fence makers.

Good fence makers make good neighbors.

Historically, brotherhood has been very scarce, like property rights… and liberty. They definitely are the path "less traveled by".

Let us go down that path. Maybe this time, on Mars, we can get it right.

 

Track 3C 1:00

On Our Best Behavior: Optimization of Group Functioning on the Early Mars Missions

Vadim I. Gushin

Institute of Biomedical Problems, Russia

Marilyn Dudley-Rowley

OPS-Alaska

2662 Montana Road

Fairbanks, Alaska 99709

It is something of an irony that a planet named for the God of War challenges mortal humans to psychosocial behaviors which may far surpass what is seen normally. Mars cannot be explored without a human presence on that planet. There is no robotic substitute for processing complicated information, making hard decisions, and solving non-standard problems. Many phenomena will be unknown and will need the intuition and the multiple perspectives of human cognition to discern them.

With a manned mission, come all the foibles of what it means to be human. Unfortunately, dysfunctional acts and events could jeopardize the autonomous, long-duration missions as Mars exploration requires. Space and other extraterrestrial environments require of people behaviors closer to zero-tolerance for deviance. This unavoidable fact calls for optimization of group functioning.

Understanding optimization calls for comprehending the occurrences and frequencies of deviance in extreme environments among teams living and working there; for baselines of optimal standards of performance still yet to be drawn; and for the diagnosis, prevention, and correction of less-than-optimal behaviors, not only on an individual basis, but especially on a group basis. Several perspectives and methods are discussed. Finally, it is contended, optimizing group functioning for the "first Martians" could lead to a higher order of behaviors conducive to international cooperation on Earth. In the conquest of Mars, we conquer ourselves.

 

Track 3C 1:30

Defining Human Parameters for Offworld Migration:

Roles and Crew Composition

James J. Funaro

Cabrillo College/CONTACT

This paper is an attempt to define and evaluate -- from the anthropological perspective -- some of the basic human factors that need to be considered in migration off world.

Anthropology, being interdisciplinary by nature, can serve as a platform for integrating all the sciences (as well as the arts and humanities) into the human experience. In constructing an overall

approach to human migration off world, an anthropological perspective, which encompasses data from past and present cultural systems, may point out some distinctions which might prove useful to current space research.

A number of factors relevant to crew composition will be addressed. For example, evidence from ethnography, history, archeology, primatology and paleoanthropology suggests that migration has always been a natural, consistent and adaptive practice of our species, constituting the usual

way of releasing recurrent pressures created by problems of politics, population or ecology. However, comparative study shows that human (and even chimpanzee) migration often consists of two separate components: exploration and colonization. Though they are not necessarily mutually

exclusive, they often occur as phases in the overall migratory process and have essentially different goals and require different skills. The need for such a distinction in a different context is already being recognized in space engineering; e.g., enabling vs. enhancing technologies.

By noting general patterns yielded by anthropological data and studying the particular cultural and ecological contexts of their exceptions, we may be able to more accurately perceive the different sets of problems (regardless of time and environment) normally encountered in various roles in the migration process and to more effectively design appropriate crews to perform their diverse functions.

Track 3C 2:00

Coping with the Enforced Intimacy of Space Flight

Lara Battles M.A

Marriage, Family, and Child Counseler

405 E. Branch St., Suite H

Arroyo Grande, CA 93420

LesCygnes@aol.com

 

As humankind pushes the limits of its habitat to stretch beyond its native planet, humans in space flight will experience unaccustomed limits to their mobility, privacy, use of space, and person and artistic expression. Interplanetary flight poses enormous challenges physically, socially and psychologically, and while Mars Mission planners are well aware of the research on these issues, the real research will be done on the way to Mars. This paper will attempt to raise some very human issues likely to arise in prolonged space flight: intrapsychic and personality conflicts, loss of mobility, sexual needs, the role of scent, and development of a functional shipboard culture.

Interplanetary astronauts must indeed be "The right Stuff," but what is right for a Mars mission may be quite different from what it meant in previous space ventures. In prolonged space flight, as distinctive on-board cultures will develop, the crewmembers will have a greater than ever need for strong intrapsychic resources and a high tolerance of enforced social contact. Personality characteristics resilient against social burnout and psychological stress may be as important to the successful mission candidate as is the design of the mission vehicle itself.

Real time contact with Earth-based controllers will diminish over the course of the mission; communications will need to accommodate to the increasing isolation and interdependency of the mission crew. Mission features and personal attributes impacting crew compatibility and capacity for self-reliance ranging form age and experience to a "sense of mission" may force a selection process wherein personalities ordinarily rejected as insufficiently aggressive might well become the crew of choice. Abilities to relax deeply, get lost in thought, or even dissociate may prove to be predictors of successful toleration of long term missions. Acknowledgement of sexuality and its psychological importance both personally and as a hormonal mitigator of shipboard rancors will prove necessary. Anyone may behave Puritanically for two weeks, but no one can deny his sexuality for the course of a Mars mission. Human pheromones are not the only scents to relive tension; use of aromatherapy may become as necessary to ship balance as regular exercise is to astronaut bodies. The Mir cosmonauts spoke of missing the "smell of green", thus evocative scent packs will support psychic shipboard balance, as will CD libraries of art, music, and even the instruments of art, creating the essence of the psyche's first aid kit. Expression of impressions and feelings through these media will provide the most economic form of psychic safety valve. A ship's counselor…or fool…might well become the critical additional crewmember when the journey across space takes years rather than months.

Longer missions not only require different logistics in planning for the long, intermittent supply line; they must also consider the more considerable physical and emotional stresses on the crew. Inquiry into these issues, choosing crew accordingly, and providing appropriate "culture support kits" will offer potential solutions which each crew will be able to use in a manner consistent with the culture it develops in flight.

Track 3C 2:30

The Case for Nurses as Key Contributors to Mars Exploration Teams

Mary Ellen Symanski, PhD, RN

Associate Professor of Nursing

University of Maine, Orono, ME

One group of people who may be overlooked as valuable contributors to Mars exploration missions are nurses. It is my contention that they would be valuable members of Mars exploration teams not only to care for injured team members, but to offer assistance to others in coping with physical and mental challenges in the environment. Zubrin contends that the engineer is the most valuable member of the Mars exploration team due to his or her ability to understand and repair sophisticated equipment. Nurses can "fix" many people problems in non-pretentious and practical ways similar to the manner in which engineers work out problems with equipment. Nurses are broadly educated yet practically trained; they are natural multi-taskers accustomed to working in stressful environments. Nursing education also emphasizes the positive aspects of human beings. Characteristics of nurses that would be valuable on a Mars expedition include: flexibility, able to handle medical emergencies, able to respond to psychological emergencies, able to deal with sticky people issues, able to improvise supplies in whatever setting they find themselves. Nurse practitioners, who have additional clinical education, are trained to handle basic health problems, and are used in health practices as "physician extenders". It is my contention that the human cargo going up to space is very valuable and as complex as the sophisticated equipment. Ingrained in the traditions of the nursing profession are the values of helping others and promoting well being and health. Nurses are "doers" as well as thinkers and problem solvers, and would readily pitch in with whatever other tasks need to be done. I believe that the contributions of a nurse on a Mars expedition would be worth his or her weight many times over.

 

Track 3C 3:00

What is Acceptable Technical Risk to Commit to a Manned Mars Mission?

Dennis G. Pelaccio

Pioneer Astronautics

445 Union Boulevard, Suite 125

Lakewood, CO 80228

(303) 980-0231/(303) 980-0753 FAX

strcspace@aol.com

and

Joseph R. Fragola

Science Applications International Corporation

7th West, 36st Street

New York, NY 10018

(212) 239-8510/(212) 239-8512 FAX

joseph.r.fragola@cpmx.saic.com

 

A number of critical sociological and technical elements must come together for a serious commitment to be undertaken for a manned Mars mission by a nation, or by the world of nations. The three required elements to commit to such a mission are: strong political leadership; the availability of the proper level of financial resources; and, lastly, the technical capability to pursue this goal. Other major elements that are not necessarily required for a commitment to a manned Mars mission, but could provide additional rational for such a mission, are: to investigate and exploit potential commercial and/or scientific payoff(s) by colonizing Mars; or the need to colonize Mars for the survival of civilization if there is a catastrophic event that takes place on Earth, such as a collision from a large asteroid. If one examines past great exploration initiatives, such as Columbus discovering America or the manned moon mission landings, the three major elements to support these historic initiatives did come together successfully. By examining these and other similar exploration initiatives, extensive insight can be gained in understanding the levels of technical risk that were considered acceptable to commit to such historic endeavors. When these initiatives were undertaken their technical risk levels were well below those typically considered acceptable for state-of-the-art aerospace systems. It is likely that because of the technical complexity and large investment required to perform a successful manned Mars mission, levels of the technical risk that are comparable to these other historic exploration endeavors will have to be accepted, if such a mission is to be undertaken in the next 25 to 30 years.

This paper will attempt to identify the level of acceptable technical risk that were associated with some of these past historic exploration endeavors, and discuss how these findings can be used as criteria to help guide the commitment decision to undertake a manned mission to Mars. Additionally, a top-level discussion on how risk management methods can be used to track Mars mission risk will also be addressed.

 

Track 3C 3:30

Man and Extended Space Flight: Mental and Physiological Factors

Dr. Bradley S. Tice

Director and Institute Professor of Chemistry

Advance Human Design

P.O. Box 2214, Cupertino, CA 95015-2214

Long term space flight has serious physiological and psychological implications. Similar to long term athletic training such issues as fitness, effective training and scheduling of training, and motivational levels become increasingly important in a microgravity environment. Studies in human behavior, gross-motor activities and perceptual stimuli that parallel regimented Olympic grade training of athletes have similar benefits to astronaut's physiological and psychological well being on extended space flights. A terrestrial working model of such a system will be discussed in detail along with its applications to extend space flight.

 

Track 3C 4:00

Who Should Go to Mars?

Paul Van Steensburg

 

This will be a presentation and discussion of who should be in the first crews to Mars. The Mars Direct Plan describes the professions of the four crew members. This presentation will propose, from a layman's point of view and in more detail, who should go on the first missions including such considerations as age, sex, types of personality as well as profession. Also, the presentation will paint a picture of daily life experiences in space and on the surface of Mars and what are some of the personal hurdles that members of the crew must be prepared for? How do we verify that we have selected the right people?

Subsequent discussion will generate a consensus and recommendation on the first crews to Mars and how we test them for what will be a long, lonely, challenging and exhilarating journey.

Track 3C 4:30

Is it Life or is it Memorex?

Why Humans are Essential for Scientific Research on Mars

P.J. Boston, Complex Systems Research, Inc., Boulder, CO and Univ. of

New Mexico, Albuquerque, NM

In science fiction films and television, there is never any doubt that LIFE has been discovered, that cures for weird alien diseases only take an hour or two to develop, or that the intrepid human adventurers manage to invent a new branch of physics every few episodes to explain the latest manifestation of intergalactic phenomena

How sad that real life sciecne is so MUCH HARDER than this! Just exactly *how* much harder it is constitutes the single most compelling reason that humans are indispensible for the exploration and study of Mars. No robotic missions that can be conceived of during the next half century or so will be able to simulate the bumbling, serendipitous, yet successful behaviors of actual field and laboratory scientists as they go about their explorations.

No matter how well-planned an experiment may be, things usually get screwed up somehow. As annoying as this is to the investigators involved, it is what research is really all about (proposal writing fictions not withstanding). The truly revolutionary discoveries cannot be inferred from current theory and experience. They are unpredictable in the most fundamental sense of the term. The only cure for the common failed experiment is to have actual irritated human beings on site to scratch their heads and swear in real time and figure it all out. This is worth the risk of human life. This is worth the bother of sending people and all their payload to other planets. This is worth the nuisance of keeping humans alive, happy, and productively annoyed on the surface of Mars!

Track 4C 1:00

Radiation Health Effects: Update

E. R. Chavez and R. J. Lipinski

Sandia National Laboratories

Albuquerque, NM 87185

Earth is protected from cosmic rays by a thick atmosphere which is equivalent to about 30 feet of water; Mars is protected by the equivalent of only four inches of water. The inhabitants of a Mars base will be exposed to much greater levels of radiation than normal on Earth during their stay on Mars, and also will be exposed to space radiation during transit to and from Mars. This paper reviews the current state of knowledge on the impact of enhanced radiation levels on health.

Early data obtained in the 50’s revealed very significant health effects when the radiation dose was in excess of 100 times the natural radiation dosage obtained in a year. However, there were no good data for levels much lower than this, especially for cancer or mutations, which can take a long time to appear. So, until better data were developed, the regulatory agencies adopted a Linear, No-Threshold model in which it was assumed that detrimental effects from radiation scaled linearly and continuously from the observed values at high doses, down to zero, with no threshold required for an effect. Forty years of data collection and observation have shown this assumption to be wrong. Numerous studies with careful controls and proper statistical analyses have determined that there is a threshold for health effects to set in, even for latent cancers. A more detailed knowledge of cell biology has revealed the biochemical mechanisms that overcome radiation effects at moderate doses. These results could have a strong positive implication for human populations living on Mars. They also are relevant to the safety and acceptability of nuclear power for space transport and surface electricity.

Track 4C 1:30

NO Means They Can Go

Thomas J. Burke Ph.D.

Integrated System Physiology, Inc.

Aurora, CO

And

Michael C. Trachtenberg, Ph.D.

The Sapient Institute

Houston, TX

A single dietary change should prevent bone loss, muscle loss, arrhythmia, mentation defects, and improve immunology in microgravity (mG). On Earth, each of these disturbances is accompanied by an imbalance between the proton (H+) load each day and the availability of nitric oxide (NO), a pluripotent gaseous compound derived from the amino acid L-arginine (L-Arg). In mG, it is probable that a reduction in the amount of NO produced each day results in an imbalance even when systemic acidemia does not occur. However, all other things being equal, acidemia exacerbates this imbalance. Potassium bicarbonate (KHCO3, 1mM/kg body weight/day) will increase blood pH by ~0.02 units, without altering serum potassium concentration. In mG, lowering blood [H+] in the presence of low levels of NO will drastically reduce bone loss and prevent muscle breakdown. Muscle loss is paralleled in loss of muscle glutamine (Glut) which provides NH3 to neutralize urine H+ ions so as to permit their excretion (as NH4+). If acidemia is prevented, glutamine remains in muscle! Finally, alkalization will stimulate the enzyme that synthesizes NO from L-Arg. Small amounts of dietary L-Arg might also help restore NO to a position of balance with H+. On Earth, NO is absolutely essential for the formation of normal sized fetuses; acidemia, and thus an imbalance with NO, causes intrauterine growth restriction. NO is also necessary for the formation of f-actin proteins which form the cytoskeleton within developing and differentiating cells. Recently it has been reported that cells flown in microgravity failed to mature, develop, and differentiate; this was associated with absence of f-actin formation. Because medium pH is buffered, these cells were probably NO deficient. As plans are laid for years long trips to distant heavenly bodies and, thereafter, for colonization, efforts to minimize bone and muscle loss and the other disturbances which occur in mG should be intensified. One solution is the engineering of artificial gravity; however, we suggest that the dietary manipulations mentioned above may provide, at the very least, a back-up system for protecting the health of space travelers in the event that mechanical problems develop. The hypothesis is easily tested with animal and human surrogates of mG and could be confirmed on Shuttle or Mir flights. Maintaining a balance between NO and H+ in mG could eliminate many of the medical concerns associated with space travel. NO could mean everything to those who do GO into space.

Track 4C 2:00

Medical Considerations in the Colonization of Mars

Dr. Thomas Alred

allredtj@ubtanet.com

The colonists themselves - the human capital of colonization - are the most important element in any Mars colonization plan. Planning for medical care, the physical and mental maintenance of the colonists, therefore must be a major part in planning the colonization of Mars.

Medical care is a major element of human endeavor, constituting up to 15% of modern economies. The infant colonies on Mars will be frontier societies however and not able to devote a high proportion of their resources to medical care. It is critical nonetheless that colonists receive optimal health care to preserve their functionality in building the colonies. This conflict can be resolved by careful planning with the object of reducing or eliminating major classes of human disease among the colonists so that scarce medical resources can be allocated to care for those conditions which cannot be eliminated, as well as to handle the medical challenges which will be unique to Mars.

Approximately three quarters of health care expenditures directly relate to life style choices. These include cardiovascular, respiratory, gastrointestinal and neoplastic diseases related to tobacco use, alcohol use/abuse, drug abuse, injudicious diet and lack of exercise. Careful planning, combined with a disciplined colonist population, could reduce colonist’s medical care requirement by at least 75%. Most infectious diseases, including those that have traditionally been the bane of mankind, can easily be eliminated. Many genetic and degenerative conditions, including most neoplasia, can be eliminated by colonist selection and/or manipulation of the human genome. This is now technically within our reach and, applied to both colonists and their off-spring, will result in the subspecies Homo sapiens martensis.

The Mars colonies will go through developmental phases, which we may call infant, intermediate and mature. The medical care requirements and challenges of each phase are considered.

Track 4C 2:30

Nutritional Supplements as Radio Protectors

Anthony Muscatello

Los Alamos National Laboratory

Los Alamos, NM 87545

Rocky Flats Environmental Technology Site

P.O. Box 4013, T130A

Golden, CO 80401

The scientific literature contains several reports that show nutritional substances, such as vitamins, minerals, and phytochemicals (plant chemicals), provide substantial radioprotective effects in animal studies. Incorporating these substances to the human diet, already voluntarily practiced by a large segment of the population, in addition to providing other favorable health effects, may also provide a radioprotective effect. This potential radioprotective effect would be very useful in mitigating the effects of occupational radiation exposure to astronauts (especially future Mars explorers), airline crews, nuclear workers, both commercial and government, and populations exposed to nuclear accidents, e.g. Chernobyl. This paper reviews the existing evidence of radioprotective effects by nutritional supplements and proposes that their efficacy be evaluated, first with animal studies, followed by human tests with astronauts and cosmonauts on long-term missions, such as to the Mir space station and the International Space Station (ISS).

Track 4C 3:00

The Effects of Variable Gravity on the Life Cycle of Tenebrio Molitor

Amy M. Davis

2172 Lyndway Rd.

Beachwood, OH 44122

amy@stratos.net

A comparative study to elucidate the effects of low, normal, and high gravity on the life cycle of Tenebrio molitor was performed. Tenebrio molitor in their larvae stage were exposed to approximately 1.5 G and 2.0 G at High Inertial Rotation Behemoth ("HIRB") centrifuge at Clarkson University. Tenebrio molitor in their larvae stage experienced short duration exposure to approximately 0.0 G on NASA's DC-9 performing parabolic flight trajectories. Tenebrio molitor exposed to approximately 2.0 G and 1.5 G first reproduced 87 days after exposure to high gravity. A high gravity control group that stayed at NASA and a transportation control group that traveled to Clarkson University, but was not centrifuged first reproduced one day later. In a small sample of Tenebrio molitor that experienced parabolic flight trajectories, after 16 days, 50% reached their adult stage of metamorphosis, compared with 80% of the control group. In conclusion, a prolonged period of high gravity had little effect on the life cycle of the Tenebrio molitor. However, the decreased maturation of larva exposed to low gravity for short intervals of time warrants further investigation.

Track 4C 3:30

Radiation Shielding on Planetary Surfaces

Denise B. Pelowitz, Andrei Belooussov, Michael G. Houts, David I. Poston, Deborah R. Bennett

Los Alamos National Laboratory

Los Alamos, NM

R. J. Lipinski, S. A. Wright, R. X. Lenard

Sandia National Laboratories

Albuquerque, NM 87185

The radiation environment on planetary surfaces will be a concern for manned missions. Significant radiation sources include galactic cosmic rays, solar flares, and (potentially) nuclear power systems. This paper will report the results of ongoing research related to estimating planetary surface doses, including the dose from secondary radiation generated by high-energy galactic cosmic rays. The use of in-situ resources as shielding will be discussed, as will the effectiveness of these shields. Methods for quickly and simply creating radiation shields from resources available on planetary surfaces will be examined. These methods may be applicable to other surface operations.

Track 4C 4:00

ESA EXOBIOLOGY ACTIVITIES

G. Kminek

ESA/ESTEC

TOS-E

Postbus 299

2200 AG Noordwijk

The Netherlands

The Microgravity and Manned Spaceflight Directorate of the European Space Agency (ESA) has initiated two studies, one in 1996 and one in 1997, in order to assess the interest and the capabilities for a European effort in exobiology research. Both science teams were composed of senior scientists in the fields of microbiology, geology, cosmochemistry and related disciplines. The first report focused on reviewing the places in our solar system that are able to harbor life or prebiotic evolution. The second report focused on an exobiology package for a Mars lander. In this second report the main idea was to find the required scientific instrumentation with which exobiology research can be carried out on the surface (or subsurface) of Mars. The concept is based on a piggy-pack payload design and not on a dedicated exobiology lander. Its scientific objectives are: to identify and characterize the oxidants, to find morphological and chemical signatures of extinct life, and to determine the chirality of organic compounds if present. Two concepts were evaluated for going into the subsurface: a self-penetrating mole design and a classical core drill system. Although the mole has some advantages, the team favored the classical drill concept. With an required drill depth of approximately 1.5 meters, a carousel like drill stem system can be used to avoid awkward storage requirements. In order to minimize ambiguities, an assembly of instruments was proposed to carry out the in-situ investigation. The instruments can be classified in two categories: first, the visual investigation of the samples (panoramic camera, low resolution microscope (0.1 mm/pixel), optical microscope (£ 3 m m resolution), and atomic force microscope) to characterize and select samples for, secondly, further investigation with spectroscopic and chemical analysis (Alpha-Proton-X-Ray spectrometer, Moessbauer spectrometer, RAMAN (with near-IR excitation), IR spectrometer, pyrolytic gas chromatograph and mass spectrometer). Dedicated detectors for the identification and characterization of oxidants as well as the quantitative analysis and determination of the isomer ratio of chiral compounds are part of the payload assembly. The whole exobiology system, including the sample acquisition, preparation and handling system has a mass of about 26 kg.

As a result of these activities, a nine month Phase A study of this multi-user exobiology package is now planned to start mid- to third quarter 1998 with European industry and scientific institutes.

In addition to that, ESA will propose a new microgravity program (following EMIR-2 and MFC) to the member states that will include elements of the exobiology package.

Track 4C 4:30

New Evidence for Life in the Viking Labeled Release Experiment

Dr. Gil Levin

 

Plenary Panel C 5:00 - 6:45

Special Panel on Biomedical Issues in Mars Exploration

Jeff Jones and Mike Stanford- Co-Chairs

NASA/JSC, Wyle Laboratories, Spacehab, Inc.

Introduction to Biomedical Issues:

Radiation

Surface Operations

Clinical Medicine Capabilities

Artificial Gravity

Human Performance/Psychological

Cardiovascular

Musculoskeletal

 

  • Radiation/Surface Operational Discussion

1) Radiation Issues in transit:

Threats:

SPE

GCR

Propulsion field

Space Radiation Environment Monitoring

Spectrum/ Dose

Bioeffects

Modeling/Simulation

2001 Robotics and follow-ons(pre-cursor missions)

Confirmation Solar Cycle changes on GCR exposure in Solar System

Validation of Transport Codes

Amelioration/Countermeasures:

Vehicle Design

Electronic component selection and location

Crew Habitation/Work Module location within vehicle to reduce exposure

Radiation shielding strategies

Materials

Safe haven

Fuel and Water tankage

Radioprotectant molecules

2) Surface Operations

Radiation Early Warning and Response Plan

Planetary Surface Science definition for appropriate Planning

Stay duration

Science objectives

Enabling Technology/ Human Performance: Man-Machine Interface

Work Schedules/Task Loading/Crew Size and Selection

Dust/Decontamination of Suit, Living Areas and Equipment

Skin, Mucous Membrane, Respiratory Irritant

Reducing nature of soil (Sample return) Toxicological Analysis

Suit Mobility/Pressure

Fatigue

Decompression Potential and Response

Maintenance

Pressurized vs. Non-Pressurized Rover

Safety

Decompression Treatment

Radiation safe haven

Human Factors

Mass/Complexity

Partial G-loading - physiologic effects for long duration operations

Clinical Capabilities Development

Telemedicine

Medical informatics

Enhanced miniaturized diagnostic aids

 

 

  • Human Adaptation to Rotating Environments: Implications for the feasibility of Artificial Gravity during Human Missions to Mars.

D.M. Warmflash, P. DiZio, and J.R. Lackner.

Ashton Graybiel Spatial Orientation Laboratory and Volen Center for Complex Systems

Brandeis University

Waltham, MA 02254.

During human missions to Mars, artificial gravity may be essential for maintaining bone and muscle integrity. A rotating space vehicle can provide artificial gravity by generating a centrifugal force that is proportional to the velocity of rotation (in radians/sec) squared times the radius but it will only be useful if humans can tolerate the unusual forces which would be present. Since short radius devices with high rotation rates produce significant Coriolis forces on linearly moving objects, early studies had suggested that, in order to avoid overt motion sickness and severe impairment of movement, artificial gravity would require a ship rotating at 3 rpm or less with a radius of, at least, 100 m. Although it was later shown that overt motion sickness could be prevented at rotation rates up to 10 rpm, the question remained as to whether Coriolis effects on human movement would be an obstacle to human activity aboard a short radius, high rpm spacecraft. Studies conducted at the Ashton Graybiel Laboratory of the effects of Coriolis force perturbations on arm, leg and eye movements, at 10 rpm (arm and leg) and 28.6 rpm (eye) rotation, have demonstrated rapid adaptive changes with repeated movements. These studies suggest that impairment of movement can be prevented aboard a rotating spacecraft as small as 10 m in radius or smaller, depending on the required gravity level, which has yet to be determined. The results will be discussed in the context of the feasibility of short radius artificial gravity vehicles and other implications of such vehicles, including gravity gradients and gait dependent weight changes. Supported by NASA grants NAGW-4031, NAGW-4375, NAGW-4374, and NAGW-4733.

  • Systems Engineering The Human Factor from a Group Dynamics And Psychosocial Perspective on a Mission to Mars

Dwight A. Holland, Ph.D.

University of Virginia School of Medicine

Charlottesville, VA 22908

Human Factors Engineering ("HFE," or Ergonomics) is a sub-discipline of Systems Engineering that seeks to optimize a variety of person-rated systems parameters. One important aspect of HFE is to evaluate not only the physical human performance requirements and limitations, but to assess the behavioral factors that affect performance as well. Good systems engineering design practices for person-rated systems should include detailed consideration of strengths and weaknesses of the human factor from a specification standpoint in all phases of the system design and mission management phases. Assuming that the physical spacecraft system components are reasonably engineered and safe from a first-order technical and human factors standpoint, the next critical level of analysis becomes the "softer" behavioral factors that affect the crew’s day-to-day performance. This is particularly true with regard to the interpersonal and group dynamics aspects of the human factor since these issues may affect crew communication, performance and safety so strongly. Typically, the crew in any isolated and confined environment ("ICE") such as this that have been tasked with accomplishing such a long-duration mission will have opportunities present themselves for individual and group difficulty at a variety of times during a mission. A key question to consider is how the crew/ground support will handle these difficulties when-- not if-- they occur. Past experiences of such difficulties from a host of ICEs tend to reveal that there are several important human factors and psychological parameters that will directly affect the systems management and successful outcome of the long-duration space mission with regard to these issues. Some of the important areas identified in this and a host of other summarized research are specifically: optimal crew selection, earth-bound family/friends/mission support structures, leadership (both on the spacecraft and back in mission control), the general task environment /work design, and the ability of the crew and overall mission management to adapt to changing or unforeseen conditions. Such mission attributes must be addressed throughout the spacecraft/mission design and operational phases while also giving consideration to maintaining a high degree of crew situation awareness, motivation, and mission performance without substantial compromises in safety. It is a tall order indeed to design such a spacecraft and mission, but one that is eminently possible with excellent systems engineering, human factors, and medical sciences being ingeniously and carefully applied.

 

  • Cardiovascular Concerns for Long Duration Spaceflight:

D. D’aunno, J Yelle, S. Hart

(NSBRI, NASA/JSC, UTMB)

The potential for severe cardiovascular alterations with short-duration space flight is minimal. Early adaptation of fluid shifts and neurovascular remodeling become a serious complication when an astronaut exposed to microgravity returns to Earth. Although not completely understood, the orthostatic intolerance, baroreflex resetting, and diminished cardiovascular aerobic capacity quickly return to preflight standards within a matter of days. Shuttle flights of less than 16 days have not been shown to promote cardiac conduction abnormalities. However, with missions of longer duration, there are three major cardiovascular concerns: 1) Cardiac rhythm disturbances, 2)Orthostatic intolerance, and 3)Diminished cardiac muscle mass.

Cardiac rhythm disturbances including ventricular tachycardia have been recorded on several occasions during long-duration spaceflight. Cardiac dysrhythmias pose a potentially lethal risk during long-duration space flight. There are many factors that could account for increased electrical instability e.g. increased sensitivity to catecholamines, or upregulation of adrenergic receptors, considering a general decrease in sympathetic nervous system activity observed during spaceflight and ground-based simulations. Environmental toxins, electrolyte imbalances, acid-base disturbances, hypoxia, and others all may contribute to cardiac conduction abnormalities. Countermeasures and effective treatment strategies are currently being developed.

While the impaired cardiovascular response to orthostatic stress seen immediately postflight from shuttle missions is highly variable among crewmembers, the severity and duration of the impairment increases with mission duration. All astronauts from extended stays in space have demonstrated severe orthostatic intolerance. The inability to maintain adequate arterial blood pressure and cerebral perfusion with tilt testing persists in various stages for days after return to Earth gravity. How people will respond to the decreased gravity of Mars after the months-long journey is not known. Understanding the complex changes in the autonomic nervous sytem resulting from exposure to microgravity and its relationship to volume and electrolyte homeostasis and vascular resistance is paramount. Local factors responsible for vascular tone such nitric oxide, endothelin and prostaglandins need to be explored in the weightless environment. Gender is also a concern with postflight orthostatic intolerance. Of the astronauts who become presyncopal after short-duration missions, 75% are female. Estrogen is known to increase activity of nitric oxide synthase and this may be one reason why female astronauts have decreased tolerance to orthostatic stress. Specific countermeasures, in addition to fluid loading and g-suits, should be developed to effectively manage long-duration mission postflight orthostatic intolerance.

There has been some evidence that long-duration stays in space are associated with a decrease in cardiac muscle mass. A recent bed-rest study has also seen a similar effect. It is not known if actual protein is lost from cardiac muscle or if the change in mass reflects a decreased hydration state. This could be one contributing factor to the decreased cardiovascular aerobic capacity to physical stress observed with exposure to microgravity. Cardiac tissue from animals flown in space reveals decreased protein concentrations, altered cytoskeletons and reduced mitochondria. While it is difficult to equate these findings with human subjects, evidence for altered myocardial cell structure and function cannot be dismissed easily. Too little is known about the effect that long-duration exposure to weightlessness may impose on cardiac tissue. Exploration of these issues is being planned for ISS.

Long-duration spaceflight presents concerns for the cardiovascular system and the health and well being of the crew, that is not seen with short duration flights. Cardiac conduction abnormalities, alterations in the autonomic nervous system, vascular endothelial changes and cardiac muscle mass decreases all present areas of study and preparation for a mission to Mars.

  • Musculoskeletal Issues for a Mars Mission: Calcium Metabolism and Orthopedic Risks, Countermeasures for Bone Loss, Urinary Calculus Formation and In-flight Contingency Plans

J. Muccio, D. Holland, J. Jones, P. Whitson, B. Pietrzyk

Jim Muccio, M.D., M.S.

University of North Carolina School of Medicine

Chapel Hill, NC 27510

OVERVIEW: A long-duration mission to Mars with a one way, 8-12 month exposure to microgravity may pose a significant risk to crew safety and mission success if appropriate safeguards and/or therapeutic interventions are not established. Bone demineralization and the potential for fracture in an otherwise isolated and remote environment may ultimately pose the greatest physical risk. Bedrest and in-flight studies have suggested that on average flight crews could loose 1-2% of bone density/month of exposure to microgravity, primarily in the weightbearing lower extremities, i.e., the femoral neck and trochanteric regions, and in the lumbar spine. Based and data thus far, no nadir has been reached and recovery to a preflight bone density upon return to a full (1g) or partial gravitational environment may be incomplete, and is poorly understood.

Osteoporosis studies suggest that fracture risk is dependent upon three factors: fall severity (direction and force), bone mineral density (BMD), and body habitus. Fracture thresholds for hip and lumbar spine BMD have been established for the osteoporotic population, and may be useful as a guide to estimate the fracture risk from bone mineral losses associated with microgravity environment of long-duration spaceflight. Exercise and pharmacologic interventions for reducing bone mineral losses and fracture risk have also been established in the osteoporotic population and may be an effective countermeasure in space. The potential for, and the severity of a fall, could be reduced through thoughtful spacecraft/ vehicle, spacesuit, and mission design as well as operational constraints. Such constraints might include a specified period of time for a cautious "ramping-up" of physical activities after arrival on the martian surface. Also included during this window of time might be a formal "work-hardening" program before full physical activities are resumed. Accurate monitoring of an astronauts overall physiologic health and the thoughtful consideration of work type and levels could reduce the potential for an orthopaedic injury.

The renal stone risk index measurements show elevated risk of urinary calculi for crew inflight and immediately post-flight. This risk has been documented by several post-flight stones in US crew and an in-flight stone in the Russian program. A comprehensive stone management program is being developed for exploratory class missions to employ a prevention prophylaxis strategy and treatment options in the event of an in-flight contingency. The study proposed for ISS supplements the existing hydration countermeasure with daily potassium magnesium citrate. A contingency management protocol has been tested and validated in 0-g parabolic flight.

Track 5C 1:00

Alh84001 and The RNA World

Dr. Julian A. Hiscox

IAH Compton Laboratory

Compton, Berkshire RG20 7NN

England, UK

Julian.hiscox@bbsrc.ac.uk

ALH84001, at nearly 3.9 Gyr is the oldest SNC meteorite and represents a time on Mars when the climates of Earth and Mars were thought to be similar. Several lines of controversial evidence have been identified which suggest that ALH84001 contains the remnants of ancient Martian

life. In addition, scanning electron microscopy revealed ovoid structures 20 to 100 nm in diameter that resemble the fossilized remains of certain types of terrestrial microorganisms. However the putative nano-fossils found within ALH84001 are an order of magnitude smaller than the smallest terrestrial bacteria. Arguments have been put forward suggesting that the nano-fossils are not large enough to contain molecules such as DNA or RNA or the enzymes necessary for their replication and thus cannot be remnants of biological structures.

Comparisons between organisms of metabolism, protein evolution and gene sequences have been used to speculate on the early course of evolution. One hypothesized route to cellular life is the so called "RNA World" in which RNA acts as both information template and enzyme, unlike most

modern day organisms where DNA is the information template. If both the RNA World and the evolution of membranous structures overlapped then RNA viruses can be used as examples of membranous biological structures with RNA as the genetic material.

Using these organisms as models of such a transition in the RNA World this paper argues that particles with diameters similar to those observed in ALH84001 could contain complex RNA genomes surrounded by a lipid bilayer. However functions such as nucleotide synthesis would

have to occur in the environment. Whilst the paper does not show that the so called nano-fossils are remnants of an ancient Martian life, the suggestion that these structures are too small to contain biologically relevant molecules is disproved.

Track 5C 1:30

Natural Transfer of Viable Microbes in Space Part 1: From Mars To Earth And Earth to Mars
Curt MILEIKOWSKY (a), Francis A. CUCINOTTA (b), John W. WILSON (c), Brett GLADMAN (d) Gerda HORNECK (e), Lennart LINDEGREN (f), Jay MELOSH (g),Hans RICKMAN (h), Mauri VALTONEN (i)
(a)	KTH (Royal Institute of Technology), Stockholm, Sweden
(b)	NASA Johnson Space Research Center, Houston, TX
(c)	NASA Langley Space Research Center, Newport News, VA
(d)	Canadian Institute for Theoretical Physics, University of Toronto
(e)	DLR (Deutsches Zentrum für Luft- und Raumfahrt), Cologne, Germany
(f)	Dept. of Astronomy, Lund University, Sweden
(g)	Lunar and Planetary Lab., University of Arizona, Tucson, AZ
(h)	Astronomical Observatory, Uppsala University, Sweden
(i)	Observatory, Turku University, Finland.
 
The possibility and probability of natural transfer of viable microbes from Mars to Earth and Earth to Mars travelling in meteoroids is investigated, including : radiation protection against the Galactic Cosmic Ray nuclei and the Solar Rays ; dose rates as a function of the meteorite's radial column mass (radius x density), combined with dose-rates generated by natural radioactivity within the meteorite ; and survival curves for some bacterial species using NASA's HZETRN transport code other factors affecting microbe survival : vacuum ; central meteorite temperatures at launch, orbiting and arrival ; pressure and acceleration at launch ; spontaneous DNA decay ; metal ion migration mean sizes and numbers of unshocked meteorites ejected and percentage falling on Earth, using current semi-empirical results viable flight times for the microbe species B. subtilis and D. radiodurans R1 The conclusion is that if microbes existed or exist on Mars, viable transfer to Earth is not only possible but also highly probable, due to the dense traffic of billions of Martian meteorites which have fallen on Earth since the dawn of our planetary system. Earth-to-Mars transfer is also possible but at a much lower frequency. 

Track 5C 2:00

Interplanetary Biological Transfer: Impact Resistance of BacteriaEntrapped in Small Meteorites

C. A. H. Roten, A. Gallusser, G. D. Borruat, S. D. Udry, G. Niederh 1,4), A. Croxatto, O. Blanc, S. De Carlo, C. K. Mubenga-Kabambi and D. Karamata.

Contact: Claude-Alain Roten

Institut de Genetique et de Biologie Microbiennes

Rue Cesar-Roux 19

Lausanne, Switzerland Ch-1005

claude-alain.roten@igbm.unil.ch

The Martian origin of at least twelve meteorites, ejected into a solar orbit after a primary hypervelocity meteorite impact and subsequently captured by the Earth, clearly demonstrate that regular exchanges of crust fragments between planets take place in the solar system. Recently described, putative biological traces in one of these ejecta led to the debated proposal that life was present in Martian surface rocks. As interplanetary transfers of biological know-how may

provide an explanation for the presence of life on at least two solar system bodies, survival in conditions mimicking final steps of interplanetary transfer of life forms entrapped in crust fragments was investigated with respect to small meteoroids.=20

From observations on the free fall of small impactors, analogous ballistic experiments can be designed and help to investigate if living cells can withstand the terminal low velocity impact. We have established that a series of different living cells survived an initial acceleration of 100 000 g and an impact in sand with a velocity of 300 to 750 meters per second. Based on these experiments and on the observation that the interior of small meteoroids remains cold during

the fall, we propose, for the first time, that various kinds of organisms entrapped in small impactors can withstand (i) the heat produced by the Earth's aerobraking, reducing the preatmospheric

velocity (usually between 10 and 70 kilometers per second) to that of a free fall (125 to 250 meters per second), and (ii) the subsequent non-explosive impact. The significance of our observations for the origin and the early development of life in the solar system will be discussed.

Track 5C 2:30

Experiments on the "Mars ISPP Precursor" Package on the Mars-2001 SurveyorGeoffrey A. Landis et al.Ohio Aerospace InstituteNASA Lewis Research Center

Geoffrey.a.landis@lerc.nasa.gov

Mars ISPP Precursor (MIP) is an experiment package designed to demonstrate on Mars the component technologies required to produce oxygen out of the Martian atmosphere. The experiment package is scheduled to fly on the Mars-2001 Surveyor lander, to launch in April

of 2001. The five experiments comprising MIP will demonstrate production of power by advanced solar cell technologies, acquisition and compression of carbon dioxide from the Martian atmosphere, conversion of the compressed atmosphere to oxygen by zirconia electrolysis, radiation of waste heat from the compression process to the night sky, and methods of mitigation of the effects of dust on the solar arrays. The package will also make measurements of the Mars

environment which will be of engineering use and scientific interest, including measuring the deposition rate, size distribution, and spectral characteristics of dust deposited on the solar arrays and measuring the spectrum of sunlight filtered by atmospheric dust in the atmosphere of Mars.

Track 5C 3:00

Rock Statistics at the Mars Pathfinder Landing Site

A. F. C. Haldemann, R. C. Anderson, N. T. Bridges, M. P. Golombek

Jet Propulsion Laboratory

Caltech, Pasadena, CA 91109

A population of some 2000 rocks was measured at the Pathfinder landing site using the NASA Ames Marsmap virtual reality system during the first 6 weeks of mission operations. Rock apparent widths and heights were determined with the Ames software. Rocks in the far-field were also

measured directly using the stereo base afforded by the Imager for Mars Pathfinder, with views from before and after deployment on its mast. Rock frequency and size distribution statistics are consistent with remotely sensed data, and with Earth analog sites. Currently, the initial 2000 rock dataset is being expanded. Additional rock parameters are being considered: shape, roughness, color, and burial. Study of this expanded database may elucidate whether, and to what extent, distinct rock populations are present at the MPF site, and will perhaps shed light on the processes that generated these variations.

Track 5C 3:30

Experimental Investigation of the Survival of Bacillus Subtilis Spores and Vegetative Cells and of Deinococcus Radiodurans, Accelerated with Short Rise Times to Peak Accelerations of 11 500´g, 17 700´g and 33 800´g

Curt MILEIKOWSKY
Royal Institute of Technology, Sweden
mil.behr@iprolink.ch

Eva LARSSON
Division of NBC Defense, FOA, Sweden

Bengt EIDERFORS
FOA National Defence Research Establishment, Sweden

Since it is now generally thought that Mars had an atmosphere, a lot of liquid water and favorable conditions for life early, it is not improbable that life appeared there before it did on Earth. If so, an interesting question is : could life have been transported from Mars to Earth inside ejecta meteoroids expelled into space by sizeable asteroids or comets impacting Mars, and by some percentage of the meteoroids later landing on Earth ? Early microbes would then have had to survive the jerk acceleration of ejecta launch of the order of 10,000´g or more with rise times £ 30ms, a thousand times faster than that in ultracentrifuges for the same acceleration. An experiment to check this, presented here, was performed at FOA's acceleration test facility using three projectiles fired to 11,500´g, 17,700´g and 33,800´g respectively and with three types of microbe on each projectile: Deinococcus radiodurans R1 and Bacillus subtilis 168 in spore and vegetative form. The microbiological loading of the bacteria before the shots , sampling and counting of the surviving microbes was done by the FOA Defense Research Establishment, Umeå, Sweden. The results showed that a large number of each type of microbe survived each of the three shots.

Track 5C 4:00

Soil Sampling on Mars

John Paterson

Lockheed Martin

john.l.paterson@lmco.com

In response to the need to develop a device for collecting and isolating soil samples for a landed Mars mission, a preliminary study was performed. This need arises from a new class of experiments in exobiology dealing with the search for organic material and the nature of soil oxidants. This work is intended as a follow on the ill fated MOX '94 experiment.

It is thought that organics may be present at some depths and locations on Mars. To analyze organics it is necessary to decompose a sample by heating it within a chamber and testing evolved gasses. The basic instrumentation to perform this analysis can be configured in several ways, but all require collecting soil inside a sealed chamber, and the ability to humidify the sample. It further requires that the sample be of a known volume and from a known depth. the soil required for these experiments may come from just under the surface or depths of several meters. The ability to capture a sample in either case as simply as possible with limited power is the context of the following study which was performed from 1992-1994.

Track 5C 4:30

A Robotic Mission to Mars Based on Three Radio-Linked Minispacecrafts

Antonio de Morais

Institute of Physics, University of Sao Paulo, Brazil

macca@cbpfsu1.cat.cbpf.br

This paper proposes a small, joint robotic mission to Mars based on three radio-linked mini-spacecraft:

One carrying a radio radar (much smaller than the one used in the Magellan Project) to map the Martian surface and perform gravity survey, and a magnetometer to measure the almost unknown magnetic field of Mars.

The second spacecraft would carry a near-infrared mapping spectrometer to sense the surface mineral composition, and a high-resolution solid state image camera (in visible light) to see the Martian surface and the cloud structure.

And the third spacecraft would carry an infrared spectrometer and a low resolution image camera to probe the atmospheric content and structure.

Each spacecraft would be made of very light, new, cheap materials, constructed via a design concept of just one entire block (with as minimum mechanical joints as possible), use chap confinable micro electronic components (as in Mariner spacecraft), have a propulsion system using micro thrusters, and the data, navigation, attitude and telecommunications controls would be handled by computer software operating as just one computer (one spacecraft having a master program and the other two with replicas - servo programs almost like the master one - so that in the case of malfunction of the master, one replica would assume the role of principal). Each computer would be networked via radio. The telecommunications to/from Earth would be done via the radio radar.

The operational mission would be of 1 Martian year.

Since the launch windows to Mars exist every 2 years, the launching of the three spacecraft could be made altogether by small rockets (Pegasus, etc.).

This mission would be cheap, with fast return, doing fundamental experiments, and with the facility to accomplish the mission goals even if one spacecraft should become defective.

Track 6C 1- 5 PM

Turning a Movement into an Organization

Mars Society Steering Committee

 

7:00 Mars Society Banquet

Mars Society Steering Committee

The Hakluyt Prize

Mars Society Assembled

Founding Declaration of the Mars Society

Open Forum: What is to Be Done?

 

 

Sunday Plenary Session 9:00

PILGRIMS TO MARS:

An Early 21st Century Mayflower Program*

Roderick Hyde and Muriel Ishikawa

University of California Lawrence Livermore National Laboratory, Livermore CA 94550

and

Lowell Wood (speaker)

Hoover Institution, Stanford University, Stanford CA 94305-6010

We consider an early 21st century analog of the Mayflower Program, i.e., a pervasively spartan approach to establishing a permanent human settlement on Mars, in pursuit of individual private purposes and for the mutual benefit of the settlers and one or more private sponsors.

Key features of this program are one-way travel for the Pilgrims on a Mayflower-like interplanetary transit vehicle just adequate for its purpose, the minimum essential ingredients necessary for human survival and presence-expansion on Mars, comprehensive acceptance of substantial personal risk in exchange for the prospect of personal significant gains, uniform determination on the part of the Pilgrims to take and hold a human beachhead on Mars and then to expand the human presence on a new world, and the imagination and enterprise of a terrestrial sponsor-entrepreneur(s).

Rocketry sufficient to send a critical mass of humans, equipment and materials to Martian soft-landing and the ability to realistically rehearse initial program-critical activities on Mars appear as the key enabling technologies for the program. Approaches to each which are consistent with the underlying program philosophy are sketched.

A roadmap from present circumstances to the establishment of the first Martian settlement is sketched, key milestones noted, and an event-driven schedule posted.

It is noted that the majority of successful ''new world'' settlements have had the basic character of the Pilgrim-Mayflower Program. Why it is not unreasonable to expect that a program of this general character will be executed during the coming quarter-century is noted.

Track 1D 10:00

Terraforming Mars and Bioartistry

Thomas Quinn

Evolutionary Theory Outreach Group

P.O. Box 510373

New Berlin, WI 53151

Global terraforming is a biotechnology that currently exists only in theory; however, it can be loosely defined as the process of altering other planets, moons, and asteroids so they can support an Earth-like biosphere. Currently, Mars is viewed as the most likely candidate to be terraformed for a number of good reasons. It should be recognized that terraforming Mars, a landmark engineering feat, would be more than just a scientific and technical triumph for humanity. Terraforming Mars would produce the greatest artistic achievement in history. The novel, self-sustainable and evolving ecosystems of Mars would be a wondrous work of living art. The bioarts are an ancient and mostly unrecognized genre of art that includes domestication, brewing, dog breeding, gardening, and landscaping to name a few examples. Bioartists use living materials (e.g. genes, cells, organisms, species, populations, communities) as their media. Unlike static paintings and sculptures, bi0oart is dynamic and can grow, change, and evolve. It is hard to draw a line between biotechnology and bioartistry as they intersect at many points. Genetic engineering could easily be use for artistic purposes. Future bioarts, like organism design (creating new life forms), will rely on the tools of modern biotechnology. All technologies are closely associated with certain aesthetics; yet, these biases are often unconsciously expressed. It is very clear that architects design skyscrapers to meet both the structural needs of buildings and aesthetic needs of people; art and technology are closely linked in many applied fields. B viewing the process of terraforming, an extremely creative act, as bioartistry as well as biotechnology, it will be easier to produce many unique Martian biomes that excel both in form and in function. Terraforming can also be considered the ultimate bioartistry because it is presented on a global scale and would incorporate many kinds of bioartistic techniques, applications and manifestations.

Track 1D 10:30

Space vs. Sport: The Case for Space

James Pruett

jamespruett@hotmail.com

Observing the closing of the Russian and American frontiers, as well as the penetration of the

colonial world by the European powers, Oswald Spengler, author of the foremost treatise on the

rise and fall of civilization, The Decline of the West, thought that the West was doomed as there

were no more possibilities for expansion. It was Spengler’s belief that without an object to strive for in space, be it the frontier or colonial world, the West would lose its dynamic quality, and its force would break down along with its reason for being. Robbed of its youth and vigor, Spengler predicted the Western world would enter a long, steep decline, similar to the passing of the glory of Rome into the Middle Ages.

Unable to imagine manned space flight and the potential colonization of other planets, Spengler saw Western decline as inevitable. But the race to the moon offered a new direction. If only for a moment, America became a frontier nation again and the astronaut was the hero of the new frontier. The moon landing in ’69 was the awesome climax of a long chain of historic events; euphoria swept the world as now almost nothing seemed out of reach or impossible. But just six years later, the Apollo-Soyez hookup signaled an end to the competitive spirit that paced our colossal reach for the moon. In addition, public sentiment had shifted and the success of the program was used as an argument that America could put an end to age old social problems if she were so inclined to.

With the decline of the astronaut, the athlete moved to ascendancy. In a 1976 poll (Ladies Home Journal), OJ Simpson outvoted Neil Armstrong and John Wayne as the most admired man in America, signaling the triumph of stadiums sports and the spectator.

 

Track 1D 11:00

Sense of the Sacred: The Martian Landscape in Visual Art

Prof. Richard Poss
University of Arizona
rposs@u.arizona.edu

Landscape painting provides a lyrical evocation of mankind's relationship to nature. How will that relationship be transformed by migration to another planet? How will the unique character of the Martian environment change that relationship, and perhaps even human nature? Renderings of

the Martian landscape reveal much about our aspirations for the red planet.  The art of space exploration and colonization shows us deeper dimensions of what we are doing and why, of 
the human need to explore and the social drive to expand  beyond the earth.  

Since the Middle Ages, visual representations of landscape and the heavens have offered important clues to mankind's role in the cosmos.  Painting especially imparts transcendent values through objects rendered in oil, tempera, or fresco.  A few examples of works of art from the "traditional" canon of art history will be examined briefly to provide a methodological context, then we will 
examine visual art directed towards exploration, colonization, and relationships between explorers and the natural environment, and the spiritual dimensions of the great enterprise.  

From medieval manuscript illustration to contemporary space painting, this optimistic and 
forward-looking slide presentation will also serve as a survey of visual art related to Mars.

Track 1D 11:30

From Bradbury to Blamont: The Science of Mars in the Arts

Michael Carroll

spaceart@power-online.net

Mars as always had a great influence upon the arts. From the pages of Swift and Bradbury to the paintings of Bonestell to the movies of George Pal, Mars has influenced the way we think, write and sing. The arts, in turn, have inspired a generation of people who have the chance to actually explore the Red Planet robotically and, one day soon, in person. This lecture will highlight a few areas of our culture that have been impacted by Mars, and will include books by such greats as H. G. Welles, Ray Bradbury, movie clips from films such as War of the Worlds, and a plethora of paintings by artists from the turn of the century to today. We will also explore the anatomy of a scientifically accurate space painting using comparative planetology and creativity constrained by the laws of science. Plan to participate in this lively chat!

Track 2D 10:00

Martian Equality

Richard A. Jones

7229 Gore Range Rd.

Littleton, CO 80127

rrjones@ucsu.colorado.edu

With the salutary successes of Pathfinder Lander and mars Global Surveyor Orbiter, Mars is a "place" rather than an inhospitable alien world. The ALF 84001 debate has also spared renewed interest in Mars. NASA, Arizona State University, The Naval Research Laboratories, and Lockheed-Martin are designing an unmanned airplane for Martian exploration and mapping. By 2011, rock and soil samples from the Martian surface will be returned to Earth.

Privatizing space exploration has also begun in earnest with serious commercial endeavors ("orbiting Hotels") planned to encourage space tourism. The "Civilian Astronaut Corps" Mayflower II is planning to launch six passengers to an altitude of 70 miles in an attempt to win the "X" Prize.

There is no doubt manned missions to Mars, followed by colonization, will occur within three generations. Yet, given the example of an 'Old World' discovering a 'New World' five centuries ago, I wonder if a similar cycle of exploration (state sponsored), colonization (driven by scientific and economic interests), settlement (leveraged by privatization), and independence (motivated by yearnings for liberty) will inevitably occur as 'Terrans' become 'Martians'. One of the questions this paper will address is Martian Equality.

Philosophical implications of humans living on Mars will create new Martian philosophical systems. From "Martian" metaphysics, epistemology, ethics, and socio-political philosophy, the human issues circumscribing Martian colonization are immense and immanent.

Who will name the Martian months? Will the mined wealth belong to Earth or be mandated by Martian Law to remain in situ? What will constitute "pollution" on a pristine world? What laws will prevent the introduction of weapons? Long before settlers have given birth to the first 'Martians', these and many other philosophical issues ought to be dialoged and taught, lest 'Martians' be discriminated against, exploited, and decide to demand their legitimate rights to be free of us.

Track 2D 10:30

The Outward Course of Empire: The Hard, Cold Lessons from American Involvement in the Terrestrial Polar Regions

Marilyn Dudley-Rowley

OPS-Alaska

In the late 1800s and the early part of the 20th century, American explorers and their supporters had a vision of the polar regions as a logical extension of Manifest Destiny. Vilhjalmur Stefansson referred to the entree into the Arctic by Euro-Americans as "the northward course of empire". Popular history would have it seem as if this vision came true. But, approximately 100 years later, we substantially fall short of these explorers’ dreams. Most American claims in the Arctic fell through, not from lack of interest by average Americans, but the lack of government sponsorship, backing, and going back on promises made. Even the purchase of Alaska from Imperial Russia was a transaction that was almost not made. In expedition after expedition, men, women, and children died in the field waiting for pick-up from ships that would never come.

Ironically, what interest there was for the Arctic eclipsed a promising beginning of interest in the Antarctic. American explorers either had to pass themselves off as foreign nationals to join the expeditions of other countries or use their own money to launch expeditions to the southern continent. Interest in aviation caused the government to establish the United States Antarctic Service (USAS) and bases were established to protect territorial claims. However, the onset of World War II drew resources away and the bases were closed, and when the United States returned to Antarctica, it was with a different strategy of scientific investigation. In 1959, twelve nations signed the Antarctic Treaty, agreeing to use Antarctica for peaceful purposes, "froze" territorial claims, and forbade new ones. The Antarctic Treaty set the tone for similar agreements among nations which dictated similar use of the entire Cosmos.

This presentation reviews lessons from American polar exploration useful to the private Mars initiative, making recommendations for the public outreach and financing of the venture.

Track 2D 11:00

Global Dialogue toward the Genesis of Life on Mars and Beyond

Bruce N. Anderson

150 Lincoln St., #3C

Boston, MA 02111

617-253-0411; h 617-695-0309

Director, Industrial Liaison, MIT

President, Earth Day USA

The universe is as it is because of 15 billion years of "dialogue" among its trillions upon trillions of subatomic particles which, in essence, continuously taps their "collective wisdom."

As we stand at the threshold of the Genesis of Life ("as we know it") on Mars - and beyond - human consciousness gives us the special privilege of being able to create a global dialogue to tap the collective wisdom of humanity that could profoundly affect how life unfolds there.

Indeed, do we even want life beyond earth to look a particular way? If so, why? If not, why not? Does it even matter what life might some day look like on Mars - and beyond - 100 years, or 10 million years from now? Will it even matter if we pay attention to these questions? Should we simply send whomever wants to go? Are there traits we might want to maximize in the people we send? minimize?

If you were one of the first 10,000 settlers, or the first 10 million, how would you expect to govern? to educate, house, clothe, and feed everyone? to conduct commerce?

This paper explores whether a global dialogue to tap the collective wisdom of humanity to ask and answer such questions is a concept worth pursuing and, if so, what such a dialogue might look like.

 

Track 2D 11:30

The Ethical Ramifications of Discovering Life on Mars

Katherine Osborne

4639 Strathern St.

Port Alberni BC Canada

V9Y 3G2

1-250-724-1854

The possibility that life may exist on Mars, no matter how minute, poses deep ethical and moral questions to humanity as we begin our journey away from Earth. This paper will attempt to address just a few of those questions. It will also provide information on Earth's culture in regards to the inherent value of life, the conflict between the expansion of human civilization and Earth's nature, and how to responsibly approach a discovery in a manner that honors farsighted human values.

What precedents have been set in human history that may help future explorers deal with the discovery of new life? How will our past behavior hinder our future reactions? In the past, we have often approached the discovery of new life with rampant exploitation, but in recent years, have come to value all life and have begun to give it a modicum of respect. Can we possibly approach a Martian situation with a clean slate? What will happen if eventually we need to colonize and terraform Mars at the expense of loss of habitat for native life forms? Should we even consider doing it?

If no life exists on Mars, these questions will not have been asked in vain, for surely life does exist in many other places.

Track 3D 10:00

Photovoltaic Power on Mars

Geoffrey Landis

Ohio Aerospace Institute

NASA Lewis Research Center

21000 Brookpark Rd., Cleveland, OH 44135

The surface of Mars is an environment significantly different from both the surface of the Earth and from orbit. Sunlight availability is modified by the presence of dust, which varies with time of year. Several models of dust effect on solar energy on the surface are available. This paper examines what we know about the environment of Mars and how it affects the design of solar power systems and the selection of solar cells for Mars surface operation.

The Mars environment is different from the environment of Earth orbit in several ways:

  1. low intensity, low temperature operation
  2. spectrum modified by dust, making it blue-deficient compared to the orbital (AMO) spectrum
  3. spectrum change with time of day and year
  4. indirect sunlight (i.e., scattered light)
  5. presence of dust storms at some times of the year
  6. deposited dust
  7. wind
  8. peroxide-rich reactive soil
  9. radiation environment during cruise and on the surface

An additional factor is the fact that mission cost considerations mean that extremely lightweight array technology is desired. Constraints due to shock and g-loading of the landing are also a factor, as well as flexure of the arrays due to wind, if a lightweight flexible array technology is used.

Track 3D 10:30

Design Considerations for a Mars Tractor

Stewart Money

273 Willow Lane #8-B

McDonough, GA 30254

csmoney@bellsouth.net

One piece of equipment essential to establishing any permanent manned facility on Mars is the tractor. For any structure larger than a single habitat module, the essentials of sound construction will make it necessary to clear, doze, grade and compact surrounding area.

The principle difficulty is the fact that any piece of construction equipment relies on pure mass to perform its duty, a fact reflected by the term "iron" which is used to refer to such machinery in general. While not a problem on Earth, this simple dead weight is just about the last thing mission planners will want to use in filling tight payload limits.

Compounding the problem is the natural tendency to use different machines for each application. On Earth, one comparatively small job site approximately the size of a four module Martian base camp will frequently use over 300,000 lb. worth of construction equipment and still take several weeks to complete.

While certainly much harsher, the Martian environment is sufficiently similar to Earth that the fundamentals of equipment design and operation will still apply. The challenge for Mars mission designers is to develop a single piece of construction equipment capable of performing all the necessary functions while keeping weight to an absolute minimum. Not to be overlooked is the fact that due to the harsh nature of the operating environment, construction equipment breaks down with alarming frequency, making safety and ease of repair a primary consideration.

This paper examines a variety of factors, including potential job requirements; design, transportation, assembly and maintenance considerations, and suggests a specific design capable of meeting these needs. Given the substantial mass which must be boosted to Mars to assemble a tractor, this paper also considers alternate use scenarios including overland transport, astronaut rescue and power generation capabilities inherent in the design.

 

Track 3D 11:00

Inflatable Structures for a Permanent Martian Colony

Marvin E. Criswell and Jenine E. Abarbanel
Center for Engineering Infrastructure and Sciences in Space (CEISS)
Colorado State University
jenine@lamar.ColoState.EDU

A permanent human-tended Martian base requires a life support system housed within a structure providing a shirtsleeve environment for human activity.  Given the current cost of transportation from Earth, the driving force dictating the design of a Martian structure is mass.  Any structure on
Mars is a pressure vessel due to the difference between the external pressure of 0.6 kPa (0.09 psi) and internal pressure, ranging between69 kPa and 101.3 kPa (10 psi and 14.7 psi), produced by the artificial atmosphere necessary to support life.  The most efficient pressure vessel for a planetary surface habitat is an inflatable structure made of thin membranes.  Discussion of the requirements of a Martian permanent habitable structure is presented as well as conceptual designs for possible inflatable structures.

Track 3D 11:30

Drilling Operations to Support Human Mars Missions

Brian M. Frankie, P.E.

Frank E. Tarzian

Scott Lowther

Pioneer Astronautics

445 Union Blvd. #125

Lakewood, CO 80228

Trevor Wende

University of California, Berkeley

Berkeley, CA

 

Water, both as a source of hydrogen and for life support, will be one of the most valuable commodities for Martian operations. Large quantities of water are available as ice at the Martian poles, but access to these sources will be restricted by the necessarily complex transport, mining, and solids handling infrastructure that is required. Drilling for subsurface liquid aquifers may provide a cost effective alternative large scale supply of water, will enable bases to access geothermal power, and will also be of considerable scientific interest. Although there is little data on the depth of Martian aquifers, it is expected that large amounts of water can be found at depths between 1 and 5 km. Terrestrial drilling operations reaching this depth are massive, power intensive industrial efforts, but some of the latest technological advances hold promise to reduce the equipment and power requirements to a level that would be feasible for a Martian drilling operation. This paper outlines the technical design of a proposed low mass Martian drilling mission capable of reaching depths of more than 1 km.

Track 4D 10:00

A Socially Supportable Mars Colonization Program

Phil Turek

7715 Newman Ave. #201

Huntington Beach, CA 92647

pturek@laedu.lalc.k12.ca.us

 

In the past 30 years, the public perception of the Earth has changed from that of a vast world of nearly limitless resources to a small planet of finite resources. The public is becoming increasingly inclined to tolerate and evaluate proposals for the colonization of Mars.

It is important to take a few lessons from the Apollo program. During Apollo, the public was merely a passive spectator. Following Apollo 11, the public quickly became bored with the program. As a result, Apollo was cancelled in 1972 with little public opposition.

This paper advances a new approach to Mars exploration, one that avoids the fatal flaw of Apollo. The key is to provide for the direct, sustained and increasing involvement of individuals and groups with the success of the program.

The project's mission statement establishes a new biosphere on the surface of Mars capable of supporting a new civilization. The project entails three phases. The first phase of the project will start preparing future colonists and ambassadors NOW. During the second phase, a manned crew is launched to Mars for a combination exploration/colonization long-duration mission. The critical third phase splits the first manned crew on Mars into a three segments: one remains on Mars indefinitely; a second that returns to Earth permanently, and a third that returns to Earth temporarily as ambassadors from the new colony on Mars. A number of innovative techniques are used to sustain public involvement throughout each phase.

Under this scenario, the first Martian ambassador to Earth could arrive as early as 2014 and be tasked with sharing Martian experiences, perceptions, and innovations with the people of Earth.

Today's students will determine if this program succeeds or fails.

 

Track 4D 10:30

Is There a SHORT-TERM Economic and Social Justification for Human Exploration and Settlement of Mars?

Robert E. Becker

131 Old County Rd., #168

Windsor Locks, CT 06096

The Space Exploration Initiative died stillborn years ago, largely unfunded, widely viewed as unfounded. While a stream of smaller, robotic missions to Mars has started, human exploration seems to have been removed from any official timeline!

This, despite the robust economy, possible evidence of ancient life in a Martian rock, millions of hits on the Mars Rover Web Site, availability of relatively inexpensive missions like Mars Direct, and energetic advocacy by luminaries like Carl Sagan. Traditional arguments - the human exploratory spirit, intellectual excitement, and economic benefits down the road - suffice for exploration enthusiasts, but are not sufficient for the general public, and especially not for their elected representatives.

Our nation has a notoriously short attention span. All these arguments pale in comparison with immediate economic and social problems. Proponents of exploration often take a "not my job" attitude towards these issues. But until we embrace them, our arguments will remain largely unpersuasive to the public.

Human beings can not be "Faster, Cheaper, Bettered" out of the process if Mars Exploration is to gain broad support. It is the very ambition of full-fledged Mars Exploration, which can provide that justification, starting in the SHORT-TERM, during the DEVELOPMENT phases. It is this scope - living and working on another planet - which can bring space closest to the person in the street, just as on the frontier of yore.

It is the responsibility of the exploration community to apply its collective CREATIVITY and formulate cogent arguments RELEVANT to those who are NOT enthusiasts. Answering the title question affirmatively will do that. The Mars Society is the perfect multidisciplinary organization to launch a CONCERTED effort to answer it. If we succeed, a new exploration initiative could be announced, not with a bureaucratic whimper, but with trumpets blaring.

Track 4D 11:00

Why NASA Might Never Launch a Manned Mission

Dr. Fred Kelly

P.O. Box 2040

Roseburg, OR 97470

 

This paper reviews the special medical problems that are expected on a mission to Mars and concludes that, although these problems are formidable, they are solvable. We can go to Mars with the knowledge and technology we have available today.

Then why might NASA never launch a manned mission to the Red Planet? In the author's opinion, the answer is POLITICS. He reviews the role that politics played during his career with NASA that began with Project Mercury and end well after the Shuttle was flying when he took up a new career - writing about space

Writers of science fiction sometimes write not to predict the future but to change it. In his new book, THE MARS JOURNALS, he describes how NASA must go to Congress each year with hat in hand begging enough funds to keep a diminishing number of programs alive for another year. When it looks as though political opponents finally get the upper hand and NASA will not survive another congressional debate, the Senator form Texas comes up with a better idea.

It's an idea that not only makes a good book, but one that might deserve serious considerations an answer to NASA's perpetual funding problems. Why not convert NASA into a non-profit international organization like the WORLD SPACE CORPORATION? It would be free of national politics. Space programs might be based on scientific rather than political merit.

NASA takes pride in its Technology Transfer Division that encourages the private use of spin-offs from space exploration. These spin-offs from NASA research have spawned industries that add billions to the national economy, but they do not put one red cent into NASA's operation budget. The proposed re-organization would change that.

A board of directors with a proven record of fiscal management would run the World Space Corporation. Applicable laws would allow it to hold patents on discoveries and inventions, collect royalties and fees for service, and market products resulting form space research as well as products that could be manufactured in space.

We cannot entertain the delusion that such an organization could initially fund itself without continued support from governments that presently support space exploration. However, if earned revenue were added to the operational budget, these funds would gradually take over more of the fiscal load. Such an organization could have a legitimate chance of eventually becoming financially sound.

NASA has served the nation well and has more than paid its own way for nearly forty years, but it is a flawed organization. Man will colonize Mars, but the red and white and blue emblem of The National Aeronautics and Space Administration will never be planted on the Red Planet.

Track 4D 11:30

The Politics of a Mars Colony

Blaine Thompson

Track 5D 10:00

SCDTL Calendar and Clock for Mars

Lance Latham
Resource Management Systems
5901 North 33rd St.
McAllen, TX  78504-5055
rms@hiline.net

The "Standard C Date/Time Library" (SCDTL), published by Miller Freeman, ISBN 0-879304-96-0, May 1998, is intended to be a standard reference in the area of computer date/time applications. The work is an integrated tool kit of data structures and functions in the "C" language, the "lingua franca" of today's machines. Comprising almost 4,200 pages, SCDTL addresses many areas, including some 30 different calendars.

The last is Martian.

The SCDTL Martian calendar is an annual solar calendar, in which the year is composed of equal 167-day quarters. Each quarter contains 3 months, configured as (56 + 56 + 55) days.

A simple leap year rule makes common years of years 2, 4, 6 and 8 of each 10 years, and makes an exception in the tenth year every 2000 years, yielding a calculated accuracy of one day in thirty-seven thousand years. The seven-day week is retained.

A linear time scale, called the Martian Day number (MD#), similar to the Julian Day number, is created for the Martian calendar, facilitating date and time calculations.

The SCDTL system also describes a clock for Mars, which uses the standard Terran second as its basis. The Martian clock day is defined as 25 hours of 53 minutes of 67 standard Terran seconds.

Compared to other proposed Martian calendars, the SCDTL calendar has numerous advantages. It is an integrated part of a huge, tested software application. Its design is based upon extensive experience with many calendars and a knowledge of those features which are psychologically and socially useful and successful, not merely technically feasible, or of interest to a handful of specialists.


Track 5D 10:30

A Terrestrial Calendar for Mars

Nachum Dershowitz

Edward M. Reingold

University of Illinois at Urbana-Champaign nachum@cs.uiuc.eduUnlike other proposals of calendar schemes for people living on Mars, ours attempts to keep the Martian date closely in tune with the weekly cycle and Gregorian calendar as employed on Earth. It combines elements of the Gregorian solar and Hindu lunar calendars. (See our book Calendrical

Calculations, Cambridge University Press, 1997.) Its peculiarity is in the not infrequent occurrence of skipped days, needed to re-correlate the Martian and Gregorian calendars, and in this respect resembles the Hindu lunar calendar.

The underlying idea is that each sol is named according to the weekday and Gregorian month/day current on Earth. To maximize the overlap between the date on Earth and on Mars, we can choose to name the Martian sol to match the date at the terrestrial international dateline when it is noon at the Martian prime meridian. In effect, Mars is treated like a time-zone on Earth, but with the date and time coinciding with changing locales on Earth.

On account of the longer sol, this scheme would have the unique feature of expunged days (like the Hindu calendar wherein a solar day is longer than a lunar day). One can go from, say, Tuesday, January 5 to Thursday, January 7, with no sol named ``Wednesday, January 6''. This would transpire 9 or 10 times a year, and can be compared with what befalls someone traveling across

the dateline.

Such a calendar would have all its units in close agreement with those on Earth. Days would be named as on Earth. Though the sol is longer than a day, the month and year would have the same mean length (in days, not sols) as on Earth. Thus it has the advantage of being familiar to earthlings and facilitates coordination with Earth. Its year, however, bears no correlation

with Martian seasons.

Track 5D 11:00

Millennium Mars Calendar

James M. Graham and Kandis Elliot

University of Wisconsin-Madison

Madison, WI 53706

 

Science fiction writers have been devising calendars for Mars since the 1950's. The first working calendar, however, appeared in Mars Scientific Model (Michaux and Newburn 1972). Gangale (1986) described a Mars calendar of 24 months which began with the landing of Viking 1 (July

20, 1976). More recent proposals include those of Zubrin (1993), Becker (1994), and Suraq (1997). Since the number of days or "sols" in a Mars year is fixed at 668.59, calendars differ mainly in the way the year is divided into months.

In our calendar the Martian year is divided into 20 months named for the Greek gods and goddesses of antiquity. Months are arranged in four groups of five months each in which the first three months have 33 sols and the last two 34 sols. The last month of the year (Zeus) has 34

or 35 sols if the Mars year has 668 or 669 sols. The calendar begins on the date of the landing of Viking 1, which is 1 Poseidon, year 0. Days of the week are named for the Sun and first six planets (Solday, Mercuryday, Venusday, etc.). Although the Martian year begins on the first day of

northern spring on 1 Eos, this special edition of our calendar, which is called the Millennium Mars Calendar, has been synchronized to the Earth calendar to cover the interval from Dec. 20, 1999 to February 1, 2002, the turn of the millennium.

Each month on the calendar features a full-color illustration, an essay on a selected feature of Mars, a brief discussion about the Greek deity for whom the month is named, and notes about events in the history of space exploration. Separate essays discuss colonization, terraforming and the Martian meteorite ALH84001. The calendar is intended to be both educational and entertaining while stimulating interest in the exploration of Mars. The Millennium Mars calendar is one of many possible forms for a Mars calendar. Future colonists of Mars will no doubt adopt a calendar

which serves their needs best in their new environment.

Track 5D 11:30

A Mars Proleptic Calendar and Sol-Date Timing ReferenceMichael Allison Goddard Institute for Space Studiespcmda@giss.nasa.gov

A new proposal for a 22 month Mars solar calendar is designed with a view to some preservation of the conventional (Gregorian calendar) context for monthly/seasonal statistics and annual time lines, with a numerical origin preceding the important 19th century observations of Mars dust storms, and

an accurately determined reference to archival sol-date chronology. A 22 month division of the Mars tropical orbit (of 668.592 solar days or sols) would permit a cognizant transferal of the familiar names and lengths of the terrestrial months to approximately the same solar season, interspersed with ten new (30/31sol) months for Mars. (e.g. "January, February, Bradbury, Clarke, March, April, May, Hypatia, Huygens, Kepler...," etc.)

The specified (C.E.2000) calibration epoch for the proposed "Mars Proleptic Calendar" (MPC) defines a sequential "Mars Sol-Date" MSD = (MJD.TAI - 51549.0 + k)/1.02749125 + 44796.0, where MJD.TAI is the Modified Julian Date, Temps Atomique International, and k a small (approximately 0.00014d or 12sec) timing correction to the as yet inexactly navigated position of

the crater Airy-0 defining the Mars prime meridian. As proposed, MSD44796.0 corresponds to Mars mean solar midnight (cf. Allison, 1997; Geophys. Res. Lett. 24, 1967) at 0 deg longitude ("Airy Mean Time") on "MPC067 Jan1" and C.E. 2000 January6.0-k (TAI) on the terrestrial

calendar-clock. 67 Mars years (44796sols) correspond to 126.02 Earth years or 59.02 synodic periods and closely represent a half-day/sol commensurability. The implied Mars Sol-Date "MSD0.0 = MPC000 Jan0.0" therefore originates at C.E.1873 December29.502 (MJD05521.502), at a near coincidence of the Earth and Mars planetocentric solar longitudes, and precedes the earliest recorded occurrence of a regional Martian dust storm in C.E.1877.

Track 1E 1:00

Mars Mission Operations

Ken Peek

15426 Pebble Lake Dr.

Houston, TX 77095

kenneth.e.peek1@jsc.nasa.gov

Although much thought has been applied to the idea of going to Mars with regard to the hardware and the Astronauts/Cosmonauts who would make the trip, not as much has been directed as to how it would be supported from the ground on the blue, not the red planet.

If NASA support is obtained, existing infrastructure can be utilized to varying degrees although conflicts with other programs (ISS and Shuttle) should be expected. If a private venture is planned, this mission support apparatus must be created. A list of this would include at a minimum:

  • Mission Control Center (MCC) including all supporting material and staffing
  • A Deep Space Network (DSN) or Shuttle TDRSS equivalent for voice/telemetry routing from the spacecraft and Martian ground sites to the Earth.
  • Launch services and ground support equipment for the launch vehicle(s).

Each item would bring a unique set of challenges to the mission. Some of these would include:

MCC

Chain of command in the control room, especially if flight is international

Console support and positions (24 hrs a day or in sync with Mars clock?). shifts, cross-training

Attrition with the control team during the flight(s)

Loops/voice protocol/common language & measurement system

Procedures needed and how retrieved (checklists, mals. etc. paper or/and electronic?)

Training (integrated sims, possibly separated by vast distances (Antarctica to Houston?))

Ground support hardware (workstations, display screens, servers, etc.)

DSN/TDRSS equivalent

Time/distance differences (relay communications lag)

Uplink and D/L channels, network availability (presumably DSN which is currently well taxed)

Launch Services

Range/pad conflicts with other programs

Regardless of whether or not NASA facilities (or ESA, RSA, etc.) are used, many of the same problems would arise. Some of these problems have been addressed in other programs, most noticeably Skylab and Mir, but may need to be re-tailored for Mars missions.

Track 1E 1:30

MARSSAT: Assured Communication with Mars

Tom Gangale

430 Pinewood

San Rafael, CA 94903

gangale@jps.net

In the past, unmanned missions to Mars have accepted the inevitable communications blackout that occurs when Mars is in solar conjunctions. This interruption, which lasts several weeks, would seem to be unacceptable during a manned Mars mission. This paper proposes a relay satellite as a means of maintaining vital communications links during conjunction, and explores candidate orbits for such a spacecraft.

The basic approach to system design is to minimize size, weight, and power of spaceborne elements of the communications system, since it is more economical to compensate with large, heavy, and power-consuming elements on Earth. Ideally, it is the Earth-to-Mars link, which should drive the overall system design, with the Earth-to-relay and Mars-to-relay links impacting system design as little as possible. This ideal is approached by minimizing the length of the link between the relay spacecraft and Mars. An orbit whose period is one Martian year, but whose eccentricity and inclination both differ from that of Mars, assures communications between Earth and mars during conjunction while minimizing the length of the link between the communications satellite and the Mars mission.

Track 1E 2:00

Using Cots Software for Mars Missions

Ned Chapin, Ph.D.

InfoSci, Inc.

Menlo Park, CA

NedChapin@aol.com

The traditional way of providing software to support space missions has been to build custom systems from scratch and then modify them to accommodate changes (the process of "software maintenance"). With the improving availability of Commercial Off-the-Shelf (COTS) software components, using COTS components extensively in building and maintaining systems is a new alternative. While we have nearly always used some COTS software components, now we can use them much more in systems associated with the exploration and settlement of Mars.

Using COTS software components has both pros and cons. The major pros can include:

  1. Lowers the cost to build and maintain the system
  2. Shortens the time to build the system
  3. Encourages the use of open standards in building and maintaining the system
  4. Eases using "spare parts" during maintenance, and reuse during development
  5. Makes component interactions more explicit
  6. Encourages encapsulation, table-drive, and instrumentation

The major cons can include:

  1. Requires either customizing the software to fit the way people want to work, or making the way people work fir the COTS software
  2. Constrains the kinds and forms of changes in systems
  3. Slows making changes in the system
  4. Adds to the diversity of styles, conventions, and practices in the software
  5. Increases the difficulty and cost of making functional enhancements
  6. Lengthens the time to find and fix performance faults and shortfalls.

Given Mars mission requirements and eventualities, achieving a balance between the pros and cons in using COTS software components involves making tradeoffs. Implementing them includes the se of tailoring code, wrappers, reuse, and certification.

Track 1E 2:30

Computerization, Fuzzy Logic and Fault Tolerance

Greg Perugini

Track 1E 3:00

Adjustable Autonomy for Human-Centered Autonomous SystemsGregory A. DoraisCaelum Research

NASA Ames Research Center

gadorais@ptolemy.arc.nasa.gov

We expect a wide variety of autonomous systems, from rovers to life-support systems, to play a critical role in the success of manned Mars missions. The crew and ground support personnel will want to control and be informed by these systems at varying levels of detail depending on

the situation. Moreover, these systems will need to operate safely in the presence of people and cooperate with them effectively. We call such autonomous systems human-centered in contrast with traditional ``black-box'' autonomous systems. Our goal is to design a framework for

human-centered autonomous systems that enables users to interact with these systems at whatever level of control is most appropriate whenever they so choose, but minimize the necessity for such interaction. This paper discusses on-going research at the NASA Ames Research Center in

developing human-centered autonomous systems that can be used for a manned Mars mission.

Track 1E 3:30

Model-based Autonomy for Robust Mars Operations

Daniel Clancy, Vineet Gupta, James Kurien, Mark Shirleykurien@ptolemy.arc.nasa.gov

Space missions have historically relied upon a large ground staff, numbering in the hundreds for complex missions, to maintain routine operations. When an anomaly occurs, this small army of engineers attempts to identify and work around the problem. A piloted Mars mission, with its multiyear duration, cost pressures, half-hour communication delays and two-week blackouts cannot be closely controlled by a battalion of engineers on Earth. Flight crew involvement in routine system operations must also be minimized to maximize science return. It also may be unrealistic to require the crew have the expertise in each mission subsystem needed to diagnose a system failure and effect a timely repair, as engineers did for Apollo 13.

Enter model-based autonomy, which allows complex systems to autonomously maintain operation despite failures or anomalous conditions, contributing to safe, robust, and minimally supervised

operation of spacecraft, life support, ISRU and power systems. Autonomous reasoning is central to the approach. A reasoning algorithm uses a logical or mathematical model of a system to infer

how to operate the system, diagnose failures and generate appropriate behavior to repair or reconfigure the system in response.

The "plug-and-play" nature of the models enables low cost development of autonomy for multiple platforms. Declarative, reusable models capture relevant aspects of the behavior of simple devices (e.g. valves or thrusters). Reasoning algorithms combine device models to create a model of the system-wide interactions and behavior of a complex, unique artifact such as a spacecraft. Rather than requiring engineers to envision all possible interactions and failures at design time or perform analysis during the mission, the reasoning engine generates the appropriate response to the current situation, taking into account its system-wide knowledge, the current state, and even sensor

failures or unexpected behavior.

We also discuss ongoing application to Mars hardware prototypes, flight tests and future research.

Track 1E 4:00

Automatic Onboard Planning and Scheduling for Deep Space Missions

Nicola Muscettola

RECOM Technologies

Kanna Rajan

Caelum Research Corp.kanna@ptolemy.arc.nasa.gov

The future of the space program calls for ambitious missions of exploration and scientific discovery. Searching for life on Mars, Europa and elsewhere in the solar system and beyond will require the solution of several challenging technical and organizational problems. A central

one is the implementation of increasingly capable and autonomous control systems to ensure both mission accomplishment and mission safety. Without these systems missions will have to be run with the current, traditional approach. This relies on frequent communication with Earth

and teams of human experts guiding step by step a mission through its tasks and analyzing and reacting to the occurrence of malfunctions. The cost and logistics difficulties of this approach, however, are so high that it cannot be reasonably carried over to the expected growth of

missions and mission capabilities. Autonomy technology is an answer to these problems.

The Remote Agent (RA) will be the first artificial intelligence-based autonomy architecture to reside in the flight processor of a spacecraft and control it for 6 days without ground intervention. The mission on which RA will fly is New Millennium Deep Space One (DS1) which has been

described elsewhere. The primary benefits of having an on-board Planner/Scheduler are twofold. Firstly plan procedures are abstract and modular and allow synchronization of high level activity very easily. Having them generated on board allows flexibility and robustness in executing sequences which are more closely tied to the run-time environment in addition to saving costly bandwidth necessitated by coverage from NASA's Deep Space Network (DSN). Secondly, an on-board planner allows a quick and robust recovery when contingencies arise (e.g recovery from faults or serendipitous science opportunities) and the round-trip communication delay prohibit faster reaction times from ground based personnel.

This paper describes the overall necessity of using such Planning/Scheduling technology, its expected impact and some technical details of the technology itself in terms that is accessible to the

general audience.

Track 1E 4:30

Autonomous Rovers for Human Exploration of MarsJohn Bresina, Gregory Dorais, Keith Golden, Richard WashingtonNASA Ames Research Center

Moffett Field, CA

richw@ptolemy.arc.nasa.gov

Autonomous rovers are a critical element for the success of human exploration of Mars. The robotic tasks required for human presence on Mars are beyond the ability of current rovers; these tasks include emplacement and maintenance of a habitat, fuel production facility, and power generator, landing-site scouting, and mining. These tasks are required before and also during human presence; the ability of rovers to offload work from the human explorers will enable the humans to accomplish their mission. The capacity for these tasks will be realized by significant advancement toward full rover autonomy and, in particular, by overcoming current rover mission limitations in the areas of robust operation, resource utilization, and failure recovery.

The Pathfinder mission demonstrated the potential for robotic Mars exploration, but at the same time indicated clearly the need for more rover autonomy. The highly interactive, ground-intensive control with significant downtime limited the effectiveness of the Sojourner rover. Advances in rover offer increased rover productivity without risk to rover safety.

We are developing an integrated on-board executive architecture that incorporates robust operation, resource utilization, and failure recovery. This work draws from our experience with the architecture for the Deep Space One autonomy experiment, with enhancements in the area of ensuring robust operation in the face of unpredictable, complex environments, such as what a rover encounters on Mars.

Our ultimate goal is to provide a complete agent architecture for rover autonomy. The complete architecture will include long-range mission and path planning, self-diagnosis and fault recovery, and continual monitoring and adjustment of execution resources. The architecture will enable robust operation over long ranges of time and distance, performing complex tasks in a planned and opportunistic manner, and serving as an intelligent, capable tool for human explorers.

Track 2E 1:00

Reassessing the Human Condition: Philosophical Aspects of Mars Exploration

Prof. Richard Poss

University of Arizona

rposs@u.arizona.edu

What does our commitment to Mars as the next human frontier do to the classic general arguments for space exploration? This paper outlines seven traditional arguments for space exploration.It examines the strengths and weaknesses in each argument. Then, it analyzes the effect of the commitment to Mars in each.

The function of the commitment to Mars is to focus and clarify these traditional arguments, bringing them down from a theoretical perch to the level of the practical and the doable.

The paper will describe several areas in which the cultural imperative to explore is given concrete fulfillment in the commitment to Mars which it did not have before.

Moving beyond the general dedication to exploration to a commitment to the settlement of Mars in particular provides more than a buttress to an old ideology. It is a communal decision which operates at more depths than a mere policy decision. The health of the human community depends on the fulfillment of such a resolution. This paper will approach these depths from the perspective of seven classic arguments for space exploration.

Track 2E 1:30

Martian Exploration and Related Terrestrial Social Returns

Donald Barker, M.S., M.A.

Gregory Chamitoff, Ph.D. (gregory.e.chamitoff1@jsc.nasa.gov)

George James, Ph.D.

According to current theories of learning and motivation, at some fundamental level of the human psyche, the drive to explore and understand the unknown influences human behavior and has the potential to be directed to ensure the propagation of the more positive aspects of modern society. Motivation is defined as an inner psychological or biological state end process which prompts, directs and sustains activity and behavior. Research has demonstrated that, for many animals, the opportunity to explore proves to be highly rewarding and reinforcing (similar to drives related to hunger, thirst and social interaction). Removal or deprivation of novel stimuli and abilities to interact within new environments can lead to heightened drive states (an aversive condition). In addition, such intrinsic responses can be developed during early formative ages and continue to maintain strong influences later in life. As a result, the connection between the intrinsic exploratory response in humans and the unknowns of space travel can be directly joined. At the time of the first Apollo Lunar landing, the capacity and potential of modern mass media was just becoming visualized as a world encompassing and entwining technology. For the first time in human history, more people were privy to a single event, as it occurred, than ever before in human history. The first missions to Mars, with the benefit of forty more years of technological and telecommunications advancement, will provide leaders and educators with an opportunity to motivate younger generations to pursue goals in science and technology and hopefully suppress fears of future social and economic stability. This material examines the potential for examining the socio-psychological consequences of the first manned mission to Mars with the objective of achieving an understanding of human motivation and modern societies ability to involve and solicit the general interests of the public with respect Mars exploration while advancing future generations pro-social behaviors and desires towards learning.

Track 2E 2:00

Mars Exploration - The Survival of Our Civilization

E.G.Petrakakis

Costa Do Dol Ltd

Box 319

Maputo, Mozambique

101754.1676@compuserve.com

Right through the history of Mankind the necessity for exploration and expansion is very clear and evident fact, this can be summarized in one sentence - our Society and Civilization needs to Explore and Expand in order to survive.

We can look at various examples including the origins of the United States and this is exactly the first reason why Mars is the key to our continuous survival. Getting there, therefore is not only about finding microorganisms or evidence of past civilizations or to test our rockets. If we look around today in the World what do we see? And if we take the last part forty years what do we see?

The same issues are being still unanswered and the greatest society dangers are creeping in -

Drugs, Mobs, Prostitution, War, Racism, Terrorism Radicalism....etc are all still here and in a big way.....and who said the Atomic Age is a thing of the Past.

So it’s simple Space Exploration with the kick off start, Mars is the channel through which, once again our civilization will expand through and develop into. By doing this we will automatically absorb our civilization will expand through and develop into, by doing this we will automatically

absorb all the Global Resources, because its new dimension and that is what it takes to get there and to live there. If our society explodes outwards we have a healthy existence if we don’t we will continue to grow and finally take over, we will move into a feudal, overpopulated polluted world.

Lets use the next century to put our old issues finally into history and move into the next dynamic of new futuristic society - let’s start with Mars and there in an intelligent way - THAT IS ABOUT SPACE EXPANSION,OUR LAST DIMENSION AND OUR SURVIVAL.

Track 2E 2:30

The Gen-X Rallying Cry? To Mars!

Gen-X Needs a Cause, and that Cause Should Be Space

George T. Whitesides

(703) 406-5955

Gen-X is the first generation in history with the chance to send one of its own to Mars. For our own sakes, as well as for the sake of humanity, we cannot let that chance pass unfulfilled.

We are a curious generation, both lucky and adrift. Blessed with prosperity, peace, and education, we are on the verge of inheriting the strongest country in the world, at one of its greatest moments. In just a few years, we will hold an unparalleled opportunity to do something great for mankind, to make a deep and lasting mark on history.

There is only one problem: as a generation, we have no grand aspiration for our future. If is true that some of us care deeply about issues like the environment or service, but is there a goal out there that we seek together, that unifies and inspires us? Corner one of us, look us in the eye, and you'll see that the answer is no.

This much-publicized ennui has its roots in the happy condition of our land. Living in a world without advancing evil, we have had the luxury of turning inward. Raised in a country in which the great injustices have been at least legally remedied, we have been left to work out the details of battle fought before our time.

With some hesitation, we admit that we wish we did not live in such uninteresting times. Privately, we yearn for a cause of our own, a grand public effort that would take us beyond the video-game society in which we have been raised.

What we have not realized is that there is a cause out there for us, one that is everything that we secretly hope for.

It is space exploration in general, and Mars in particular.

Making space our cause, and Mars our goal, would bring us together under a grand, peaceful endeavor. It would teach us about our universe in ways that we can barely imagine, and it would spur technology to greater heights. It would be a great gift to our children, bot for their education and their future. To send some of our own to Mars would transform us from a generation that history will forget into a generation that history will revere.

Space is the next frontier of humanity, and we are the next generation. Mars, an uninhabited planet whose environment is closest to our own, waits, empty, for our arrival. If ever there was a match made in heaven, this is it.

Track 2E 3:00

A Shining City on a Higher Hill: Lessons from the Last Colonization of a 'New World'

Rev. James D. Heiser

Publisher, Repristination Press

3555 Plover Drive, Decatur, IL 62526

The colonization of the New World provides examples of three possible motivations for colonization of Mars: (1) military expansion or competition between colonizing nations, (2) economic exploitation of the natural resources of the colony, and (3) pursuit of political and religious freedom. The first motivation, international competition, played a crucial role in the early development of the Soviet and American space programs, particularly in the race for human exploration of the Moon, a situation roughly analogous to the competition between Spanish, Portuguese, French and English colonization efforts in the Americas. However, the end of the U.S. - Soviet 'Cold War' eliminates this motivation for colonization of Mars, although some experts hope that cooperation between the two nations might yield exploration of mars, a crucial preliminary step to colonization. The second potential motivation, economic benefit, is even more tenuous, since the success of such an approach rests on profits from hypothetical scientific advances or economically feasible exploitation and/or exportation of Martian natural resources, while relying on a transient population of workers motivate by a desire for a quick profit, not permanent settlement. A similar situation can be found in the early Virginia colonies that were financially disastrous until he beginning of the exploration of tobacco and the importation of slaves. The third motivation - freedom - is the most fruitful motivation for colonization in terms of stability, steady growth, and cultural cohesion. The desire for religious self-determination was the guiding motivation for successful English settlement in New England, efforts that were initially quite meager in terms of personnel and financial resources. The pursuit of freedom - particularly religious freedom - is a motivation powerful enough to move men and women to leave behind land, home, family - even a world - to build a new life.

Track 2E 3:30

Benefits of Opening a frontier

Eldon Gatlin

225 North Fenceline Dr.

Tucson, AZ 85748

EldGat@symix.com

This paper will present the social, economic, and political benefits of opening up a frontier. History is full of examples where individuals, groups, and whole civilizations have relocated either forcefully or by choice to unsettled locations where they flourished anew to become thriving, and in many cases, over time, dominant cultures/economies. In addition almost ever culture or country that has pushed into uncharted territory has seen their economy soar and prosperity extended to all

levels of the sponsoring entity.

In addition some of these forcible immigrations of less desirable aspects of the parent societies' individuals have spawned new ideas, cultures, and economies that are the driving force of the world as we know it. Some were by choice between incarceration and a hostile environment. Others were a chance to practice their beliefs or face suppression. These kinds of relocations have had a double benefit. In both cases, the individuals involved gained a chance and the ejecting party no longer had to deal with the perceived problem of the ejected. The English were very glad to get rid of certain social entities from there midst at various times.

Some of the things we are seeing in society is due to the fact that the pioneering spirit which lead to survival has been redirected or channeled into behavior that is socially non-conducive to all parties

involved in interaction. No longer can an individual go out and avoid situations that cause problems. They fall under scrutiny from the government, neighbors, or society. Think if the Pilgrims would not been able to come to a new place and institute their beliefs and practices.

Where would the world be today?

Track 2E 4:00

Civilizations at the Crossroads: The Historical Need to Explore

Wayne Bowen

Track 2E 4:30

The Likely Influence of the Martian Frontier on Technological Progress

Prof. Vernard Foley

University Hall

Purdue University

W. Lafayette, IN 47907

Several historical examples from the middle 1700's onward support the idea that frontier conditions, by crating local labor shortages, drive up wages and thus promote mechanization.

First glimpsed in part by such observers as Franklin, Hamilton and Adam Smith, the theme achieved extended discussion in H.J. Habakkuk, American and British Technology in the 19th Century: The Search for Labour-Saving Inventions. Though criticized by such as Temin, the theory remains a basic starting point. Later analysts such as Rosenberg, Smith, Hounshell and Hoke, have built upon it.

The crucial case has been American gun making during the early national period, culminating in the achievement of interchangeable parts manufactures, first in government armories by John Hall, et. Al., and later in private firms such as Colt's Hartford Armories. The latter derived partly from prior changes in the edge tool industry, and study by the author indicates that the redesign of the axe in America can be correlated with efforts to extend the productivity of the timber processing labor force.

The paper will also address such other cases as the balloon frame house design, the Pennsylvania long rifle (author's work) and the origins of several metal and woodworking machine tools, such as the famous woodworking patent of Samuel Bentham.

Frontier conditions may also have played a role in stimulating French interchangeability efforts. Experiences during the French and Indian wars pointed to the deplorable contrast between the ponderousness of European martial ways, and the native "skulking way of war". Work in progress indicates thus far that distance from resupply sources (in the settlements) promoted the engineering ideal of interchangeability. Hence, if the laws of economics apply interplanetary, Mars should see a further spurt in human-centered technological change.

Track 3E 1:00

The Heatpipe Power System (HPS): a Near-Term, Low-Cost Space Fission Power Supply.

Michael G. Houts, David I. Poston, and Deborah R. Bennett

Los Alamos National Laboratory

Los Alamos, NM

Marc V. Berte

Massachusetts Institute of Technology

Boston, Massachuesetts

The Heatpipe Power System (HPS) is a potential, near-term, low-cost space fission power system. The Heatpipe Bimodal System (HBS) is a potential, near-term, low-cost space fission power and/or propulsion system. Both systems will be composed of independent modules, and all components use existing technology and operate within the existing database. The HPS and HBS have relatively few system integration issues; thus, the successful development of a module is a significant step toward verifying system feasibility and performance estimates. A prototypic HPS module was fabricated, and initial testing was completed in April 1997. All test objectives were accomplished, demonstrating the basic feasibility of the HPS. Fabrication of an HBS module is underway, and testing should begin in late 1998. The presentation will provide a system description in addition to pictures and results from the test program.

 

Track 3E 1:30

Utilizing the Heatpipe Power System (HPS) on the Surface of Mars

Dave Poston

Los Alamos National Laboratory

Los Alamos, NM

The Heatpipe Power System (HPS) is a passively safe near-term low-cost space fission power system (SFPS). An SFPS is defined by three important attributes: 1) high specific power (power/mass)—otherwise it would not be economical to launch the system off the Earth, 2) reliability—because there is little or no hands-on maintenance after the system leaves the Earth, and 3) safety—because the system must remain safe while it operates, and while it is transported to its final destination (launch accidents present a unique hazard). These three attributes are also of primary importance for a system designed to operate on the surface of another planet (other than Earth), moon, asteroid, or comet. Such a system might best be classified as a terrestrial SFPS. There are several differences between an SFPS designed for terrestrial and space applications; these differences include: materials compatibility, heat rejection, shielding, reliability, and safety. Materials compatibility and heat rejection issues are effected by the presence of an atmosphere. Shielding issues can differ due to the presence of indigenous material and/or vastly different shielding requirements. Reliability and safety issues can be effected by how the system responds to seismic, meteorological, and astronomical events.

This paper focuses on the effect that material compatibility issues might have on the design and performance of the HPS. An SFPS is usually designed with refractory metals, because of their high temperature capability, high thermal conductivity, and in some cases better neutronic characteristics. The baseline HPS is designed to use niobium 1-zirconium, molybdenum, and/or tungsten depending on the application. One major drawback of refractory metals is that they tend to corrode very easily, thus their use in an atmospheric setting may be limited. Although the Martian atmosphere is relatively benign (mostly low-density CO2) as compared to Earth, materials compatibility will still be a major issue. Several materials compatibility test will have to be conducted, but it may be that a super-alloy based SFPS ( possibly stainless-steel or Inconel) will be required on the Martian surface. If a super-alloy SFPS is required, then the power output of a given system will probably be lower than for a refractory metal counterpart (because of lower temperature limits and thermal conductivity). One advantage of a super-alloy system is that it should have a lower development and unit cost (due to lower material cost, easier manufacturing, larger material database, etc. ); but because of lower performance, the actual cost per watt delivered to space will probably be higher. The power reduction of a specific HPS design may be up to a factor of two (in the worst case) as compared to a similar refractory metal design. However, it should still be possible to economically design and build a super-alloy HPS that can deliver 50-150 kWe on the Martian surface

Track 3E 2:00

Comparison of Mars Surface Power Options

R. J. Lipinski, S. A. Wright, R. X. Lenard

Sandia National Laboratories

Albuquerque, NM 87185

M. Houts, D. Poston, D. Bennett

Los Alamos National Laboratory

Los Alamos, NM

A Mars base will require a substantial amount of reliable power in order to ensure the safety and well being of the base personnel and to minimize the total mass of supplies needed. This paper reviews the various surface power options and lists the advantages and disadvantages of each. The power level needed is expected to be between about 50 kW electric (kWe) and 1000 kWe, depending on the activity level of the base. The higher power levels provide more margin for crew safety and allow nearly closed-cycle living plus in-situ production of rocket fuel for the return flight. The specific options reviewed are solar panels, a radioisotopic power systems, and several types of small research-sized nuclear reactors. The reactors considered include configurations which are heat-pipe cooled, gas cooled, and water cooled. The level of maturity of all of these systems is discussed.

Track 3E 2:30

Surviving on Mars without Nuclear Energy

George James, Ph.D.

Gregory Chamitoff, Ph.D. (gregory.e.chamitoff1@jsc.nasa.gov)

Donald Barker, M.S., M.A.

 

The development of economical strategies for the first human mission to Mars has increasingly focused on the utilization of in-situ resources for providing required supplies for life support, surface mobility, and the return-to-Earth capability. It has been demonstrated that mission robustness and affordability can been drastically improved by "living off the land." The Mars Direct plan and elements of the NASA Reference Mission illustrate the importance of this concept. A common feature to most mission plans, however, is the transportation of a nuclear energy source to the Martian surface. While this may be the simplest short-term solution for meeting the energy requirements of a human base on Mars, it also has the potential to be the show-stopper due to the current political climate regarding the safety of launching nuclear materials and/or polluting another planet with nuclear waste. The objective of this paper is to present alternative means for providing energy on Mars through the understanding of the local environment and subsequent utilization of these resources. The potential for exploiting solar energy on Mars is well established. However, the cost is high and the implementation involves certain obstacles, such as reduced output during Martian dust storms. Areothermal energy is a potential longer-term resource that could be plentiful in certain regions, but the utilization of this resource requires further remote sensing data as well as subsurface drilling or other surface based exploration. Wind energy has surprising potential for Mars due to the magnitude of geological features and temperature extremes that can produce reliable and strong local winds. This paper presents a summary of the current knowledge of solar, wind, and areothermal energy resources on Mars. A discussion of the means to identify these resources and the studies required in the near future to further characterize their distribution and abundance is given. Techniques that could be employed on robotic surface and orbiter missions are discussed in the context of providing information that could be used to design an energy extraction and storage system. This system would be based on a combination of solar and wind energy coupled with a liquid fuel storage system. The identification of ideal landing sites from the perspective of robust energy supplies is also addressed. This paper proposes that the production of energy on Mars, solely from local resources, may be practical enough to render a small outpost completely self-sufficient. The addition of in-situ energy resource development, to that for life support and transportation, would enhance the robustness of an initial mission and potentially advance the development of permanent human colonies on Mars.

Track 3E 3:00

Martian Power

Micky Bagdero

PSC #7 Box 992

APO, AE 09104

Martian Lasers

Power on Mars may be available from a source unavailable on Earth: solar powered carbon dioxide lasers. Carbon dioxide makes up 95 percent of the Martian atmosphere. Carbon dioxide lases in the low infrared. Sunlight stimulates carbon dioxide and causes lasing naturally. All that is needed for a power source are mirrors to focus the laser light into a beam.

The infrared laser can be aimed at a conventional boiler-turbine system for electricity. Two laser mirrors may weight a tenth as much as a nuclear reactor for the same power.

Terraforming

The temperature of Mars is cold enough to freeze carbon dioxide out of the atmosphere at the poles. Warming may be possible artificially using greenhouse gasses. Carbon dioxide is a natural greenhouse gas, and is necessary for keeping Mars warm. A possible artificial greenhouse gas for terraforming Mars is perfluoromethane (CF4). Perfluoromethane can be made from atmospheric carbon dioxide and Martian flouride minerals.

Laser Chemistry

The fluoride-perfluoromethane reaction takes a lot of energy; two kilowatt-hours per kilogram of perfluoromethane produced. It is worse for the fact that it cannot normally be achieved in one step, but requires many steps. Each step loses energy, until as much as five kilowatt-hours per kilogram are used.

Martian lasers may be able to make perfluoromethane in one step, by chilling the fluoride below the freezing point of carbon dioxide, adding powdered, frozen carbon dioxide, then flash heating the mixture, using the lasers.

Conclusion

Solar-pumped carbon dioxide lasers hold potential as a power source on Mars. These lasers can be used for producing electricity through the use of conventional steam turbogenerators. Although locations of fluoride deposits are currently unknown, terraforming Mars using perfluoromethane may be an important future use of Martian lasers.

 

Track 3E 3:30

Fusion and Martian Terraforming

Dr. Mitchell R. Swartz

JET Energy Technology

Planetary SETI Society (SPSR)

mica@world.std.com

Given the presence of water-ice on Mars, its role as the fuel in fusion systems should be considered for its benefits. Heat, electricity, water, oxygen and other raw material resources could be of vital importance.

On Mars, the available water-ice for colonists includes the tiny evanescent early morning, fog coating over rocky terrain, especially the extruded permafrost released from below the surface following meteor impact, and the several kilometer thick deposits near the poles. Orbital imaging analysis suggests large amounts of water-ice for use in fusion systems on the surface of Mars, present in the form of permafrost located near Yuti-type craters above 40 degrees north latitude. At those locations, the harvest of low nuclear weight fuel for fusion systems becomes feasible.

Fusion systems would also enable the mining of the Martian moons for their carbon and other resources. Additional benefits occur from the heat generated from the fusion generators which will enable obtaining additional water ice not only for additional fuel, but also for human consumption and use. The generation of excess amounts of water over that which is needed has the extra benefit of being available to liberate molecular oxygen to the Martian atmosphere.

Track 3E 4:00

A Stepped Approach to the Moon and Mars

Jim Bickford

jbickfor@emerald.tufts.edu

With the eventual goal of settling both the Moon and Mars, a carefully planned and stepped approach should be utilized. The first steps involve modifying space station components and off the shelf technology to create a simple manned spacecraft that will make a quick flight to Mars and rendezvous with supplies previously orbited about the planet. The vehicle will return to Earth where it can be partially reused for several subsequent missions. Human flights to Mars will not only provide public motivation for continued development of space but also the strong technical background required for subsequent success. A better understanding of Phobos and Deimos as well as the Martian environment will provide engineers of future missions the information needed to properly utilize the natural resources of the planet and avoid the costly approach of bringing everything from Earth. After the completion of the initial human Mars exploratory sequence, flights to Mars will be temporarily suspended and the focus will turn to the moon. During the moon development period the data gathered from the Mars missions could be thoroughly analyzed. This detailed analysis will funnel the eventual focus of Mars exploration. In addition to the science obtained from Moon exploration and development, the resources of the moon will eventually be utilized in future space endeavors.

Track 3E 4:30

Affordable to the Individual Space Flight

Eagle Sarmont

P.O. Box 382

Wrightwood, CA 92397-0382

cocorico@wrightwood.net

A new concept in space transportation that makes use of a Turbo-Rocket Ramjet Scramjet powered Spaceplane and an Earth Orbiting Elevator that can be built with today's materials.

It is an evolutionary system that starts with a commercially viable stage and a half to orbit Spaceplane that launches satellites and astronauts into low Earth orbit. This is followed by the addition of an Earth Orbiting Elevator which allows us to eliminate the small expendable upper stage from the system, making the Spaceplane into a Single Stage to Orbit vehicle. The next step is about how the Earth Orbiting Elevator will allow us to return to the Moon to stay and how it will further reduce the cost of living working and traveling in space by allowing us to start making use of Lunar resources. Once the Lunar base is in place the next step will be the building of an L-5 shipyard where Satellite Solar Power Stations, Space Colonies and Mars Exploration/Colony ships will be built. NASA representatives have described this system as, "The first idea we have seen that offers a believable path to $100/lb to low Earth orbit."

Track 4E 1:00

Rolling on Martian Air - The Forgotten Axis

W.Klimkiewicz

ITT Aerospace/Communication Division

wklimkie@acdNJ.itt.com

P.Zemany

Sanders, A Lockheed Martin Company

pzemany@sanders.com

In this paper, we would like to describe the need for manned and robotic aerial reconnaissance and air transportation on Mars and the problems involved in providing this capability. Some time in the future, humans will arrive on Mars. Exploration will be the most important task for the first colonists in which aerial flights will be of great value. There are no roads or airstrips to support Earth-like takeoffs and landings. Finding limestone on Mars and starting production of concrete seems very unlikely, and so some other means of building large hard structures and surfaces will be necessary. This will take time and, until then, the exploration mission must proceed. This is one reason that vertical takeoff and landing (VTOL) aircraft will be necessary on Mars. In case of engine failure, an aircraft traveling over uncharted and rugged territory, far from a base station, has to be able to make a safe emergency landing. This improves the survivability of the flyer, and the vehicle. The problem with a VTOL solution is that it is equivalent to building a helicopter that can fly at a 30 km altitude (~100,000 ft.) on Earth, where the atmospheric density equals that of the Martian surface. The power requirements on such a helicopter would be enormous. Fortunately, on Mars, due to reduced gravity, an aircraft needs only one third of the lift required on Earth. In addition, the helicopter is not the most power efficient way of hovering. In this paper, we would like to prove that there are other methods of creating lift that are several times more efficient than a helicopter. We will try to convince the aerospace community that with a propulsion system based on an "Air Paddle Wheel" which rotates around the horizontal axis, it is possible to build a power efficient, all-purpose Martian air vehicle capable of vertical takeoffs and landings, which can hover, power glide and roll on the ground.

 

Track 4E 1:30

Design of a Nuclear-Powered Rover for Lunar or Martian Exploration

Holly R. Trellue, David I. Poston, and Rachell Troutner

Los Alamos National Lab

Los Alamos, NM

In order to perform more advanced studies on the surface of the moon or Mars, a rover must provide long-term power up to or above 10kWe. However, a majority of rovers in the past have been designed for much lower power levels (i.e. on the order of watts) or for shorter operating periods using stored power. Thus, more complex systems would be needed to generate more power. One possible design for a more highly powered rover involves using a nuclear reactor to supply energy to the rover and material from the surface of the moon or Mars to shield the electronics from high neutron fluxes and gamma dose rates. Typically, one of the main disadvantages o fusing a nuclear-powered rover is that the required shielding would be heavy and expensive to include as part of the payload on a mission. By obtaining most of the required shielding material form the surface of the moon or Mars, it would reduce the cost of the mission while still providing the necessary power. This paper describes the basic design of a rover that uses a Heatpipe Power System as an energy source, including the shielding and reactor control issues associated with the design. It also briefly discusses the amount of power that can be produced by other power methods (solar/photovoltaic cells, radioisotope thermal generator (RTGs), DIPs, laser techniques, and the production of methane form the surface of mars) as a comparison to the Heatpipe Power System.

Track 4E 2:00

Autonomous Flying Robots-The Next Step for The Systematic Mars ExplorationF. Cojocaru, C.D. SavaRomanian Center of Inventics, Bucharest

A. Jinaru

Romanian Ministry of Research and Technology, Bucharest

G. Savu

National Institute of Turbomachinery COMOTI, Romania,

email: comoti@kappa.roA low-cost class of exploration robots using the in-situ, non-chemical propellant is proposed for the precursor missions, preparing the human landing on the Mars surface. The actual rovers designed to explore the surroundings of the landing site have a short radius of action and a limited life duration. A long endurance power production and propulsion system was proposed for the endowment of the Martian robots. The photovoltaic cells transform the solar radiation in electrical energy used to compress the rarefied Martian atmosphere (95% CO2) in a storage pressure tank. A high performance, multistage gas compressor , driven by a d.c. electro-motor is used to obtain the desired pressure1. If the compressed gas is expanded through nozzles, the lifting and command force are obtained for controlled flights of the robot over the rugged Martian soil. This type of vehicle was named "Mars Jumper" 2. If the gas from the pressure tank is released in a turbine, the produced mechanical power can drive the rotor of a helicopter as a Martian exploring vehicle with vertical take-off/landing capabilities3. The upper side of the rotor blades may be used as the support for photovoltaics . The distances covered by a Martian flying robot moved by this propulsion system are of order of kilometers versus the tens of meters of the actual rovers. During the survival periods (Martian nights and sand storms) the d.c. electro-motor, working in the reverse mode (as a generator) produces electrical power necessary for the data transmission to the Earth. In fact, the proposed system collects in time the existing disposable energy on the Martian surface and during a short period, the energy transformation produces high power necessary for the vehicle propulsion. The cycle is repeated by a new pressure tank charging. The proposed concept is feasible with the actual technology, without exotic materials and components, ensuring for long term the possibility to explore large areas of the Martian terrain. A flotilla of 6 or 14 robots can be launched with a single spacecraft of Titan class.

References

1. Savu G. "A Non-Chemical, in-Situ Propellant for the Martian

Machines", AIAA 95-2793 Paper, 1995.

2. Savu G. "A Low-Cost Jumper for the Martian Environment Exploration',

Acta Astronautica, Vol. 35, Suppl., pp. 699-708, 1995.

3. Savu G., Trifu O. " Photovoltaic Rotorcraft for Mars Missions",

AIAA 95-2644 Paper, 1995.

Track 4E 2:30

Mars Surface Transportation: Is Flying Cheaper Than Building Roads?

Tony Rusi

earthflight1@yahoo.com

An motorized propeller-driven ultralight aircraft, with a lifting-gas-filled parafoil wing, with a span on the order of 120 meters, is proposed for initial use in Martian exploration in lieu of four wheel drive pressurized cab vehicles. These "bush plane" analog's would require no Martian surface improvement to operate during the first phase of surface exploration. Many areas of high scientific

interest, chasms and mountain tops, of the surface may be only reachable with such devices. High average airspeeds versus ground based vehicles would also cut life support costs on sorties.

Track 4E 3:00

Mobility of Large Manned Rovers on Mars

George William HerbertRetro Aerospace

gherbert@crl.com

A study of a number of earth analogs for large, heavy, long range off-road vehicles generates useful

inputs for rover design on Mars. An investigation into the types of suspensions available, wheeled and tracked, looks at their suitability for Mars use. Analysis of the mechanics and dynamics of power requirements indicates that motive power for a given speed should scale with the local gravity. Relative stability and mobility of vehicles are examined and the lesser stability

of Mars vehicles quantified and shown to be within workable limits. Rover propulsion options are examined, investigating characteristics of possible fuel cell and internal combustion power-trains. Finally, three sample long range expeditionary rovers are described with estimated traverse ranges of over 5,000 km.

 

Track 4E 3:30

Long Range Surface Traverses During Early Mars Missions

Frank J. Crary Retro AerospaceLong (hundreds of kilometers) surface traverses will be an important part of early manned Mars missions. Previous estimates (e.g. Zubrin 1992) considered pressurized rovers capable of 500 km (?) traverses and speeds of up to ? km/hr. We present an analysis of pressurized rovers using a tractor-trailer configuration. We find that the tractor-trailer configuration allows more convenient dual-use (e.g. of the trailer alone, as soil-moving machinery at the landing site) and that significantly slower speeds are desirable for engineering and safety reasons. Slower speeds would not reduce the scientific value of the traverses. In addition, the tractor-trailer configuration

allows the deployment of in-situ fuel processing plants at remote locations. Later traverses would use these stations to refuel and the range of these subsequent traverses to travel much farther from

the landing site that is commonly assumed. The size of the fuel stations required is on par with the needs of unmanned sample return missions using in situ fuels. As a result, the development costs of the stations would be low, due to commonality with previously developed systems. The establishment of fuel stations by an initial mission will allow subsequent missions to land at the same site (thereby building up a base) while allowing access to diverse, distant regions of high scientific and public interest. This approach would enhance the value of these missions, without

increasing their cost.

Track 4E 4:00

Mars Gas Hopper: A key Component for Mars Surface Transportation

Robert Zubrin

Pioneer Astronautics

445 Union Blvd. #125

Lakewood, CO 80228

Mars ballistic hoppers with ranges up to 50 km can be developed using cool CO2 as propellant. A sorption pump is used to acquire CO2 from the atmosphere, which is then stored in the propellant tank at high pressure in the liquid phase. When flight is desired, the liquid is flashed into gas and then expanded out a supersonic nozzle, either cold, or after mild heating in a warm pebble bed heat exchanger, such "gashopper" systems could be very useful for robotic Mars exploration as they are not limited by Mars’s rough surface terrain and can be readily refueled each time they land. With the aid of gashoppers, a single suite of instruments can be made to visit a large number of widely separated surface locations, thus greatly increasing mission science return.

Track 4E 4:30

Airborne Science Platforms for Martian Exploration (or, Basic UFO Design

Considerations)

David Hall

NASA Ames Research Center

Moffett Field, CA

The presence of an atmosphere on Mars provides planetary scientists with the opportunity to extend their coverage for robotic exploration. In this brief talk, Mr. Hall will discuss basic design considerations for the design and development of atmospheric science platforms for Martian missions including similarities and diferences with terrestrial applications. He will highlight aerodynamic and propulsion requirements and will give an overview of the Mars Flyer development programs he's been involved with at NASA/Ames Research Center since the summer of 1996.

Track 5E 1:00

 

Holes in the Ground:

The Promise of Cave Biology and Subsurface Exploration on Earth, Mars,

and Beyond

P.J. Boston, Complex Systems Research, Inc., Boulder, CO and Univ.

New Mexico, Albuquerque, NM

Over the course of the next century, humans will land on and explore other bodies in our solar system. Our studies of exotic lifeforms in Earth's caves, our work on subsurface environments for life on Mars, and the potential for long-term preservation of microbial life in non-planetary bodies like comets and asteroids have led us to conclude that subsurface cavities on rocky bodies (including planets, moons, asteroids, and comets) will be an important target for exploration and scientific investigation by human missions. Not only are these subsurface environments important scientifically, but they may also provide natural sheltering structures for humans on suitable planets, moons and asteroids.

We will briefly discuss the exotic microbial ecosystems of Earth's subsurface and the bizarre means by which they make their livings (dissolving rock, living in sulfuric acid, scavenging energy from inorganic chemical reactions, etc.) We will then consider the possibilities for such communities to exist in the deep subsurface of Mars including possible methodologies for finding and studying them. In addition, we will touch on potential cave-forming mechanisms on Mars ranging from lava tubes to carbonate and non-carbonate dissolution of various rock types both sedimentary and igneous.

Lastly, we will turn our attention to the potential for buried life in other rocky bodies. This life could be in the guise of tiny passengers hitching a ride from one part of our solar system to another (e.g. Mars to Earth), microbial life from a distant solar system transported to another stellar system, or even US as we find ways to utilize natural cavities for human life support on Mars and beyond.

Track 5E 1:30

A Novel Space Transportation Concept Designed to Reduce Per-Mission

Costs for Repeated Travel to/from a Celestial Body

Dr. Stephen Heppe

Telenergy

19022 Guinea Bridge Rd.

Purcellville, VA 20132

steveheppe@aol.com

Part of the expense associated with deep-space mission derives from the inefficiency of chemical propulsion, the large amounts of fuel and propellant required to achieve mission-necessary delta-V, and the need to carry all consumables from the start of the mission.

We propose a new space transportation paradigm, which relies on the buildup of certain space "infrastructure", to minimize per-mission cost. Making a comparison to 19th century travel across North America, this is similar to replacement of Conestoga wagons with the Trans-Continental Railroad.

The infrastructure we propose is a set of man-made space stations of man-modified natural celestial bodies (e.g., small asteroids), maneuvered into a set of useful orbits, and equipped with electromagnetic launchers (railguns) as well as human habitats, depot facilities, power systems and orbital maneuvering systems (e.g., electromagnetic thrusters). On each space station or asteroid, the railgun allows small mission vehicles (spacecraft) to achieve large delta-V’s in short time without consuming onboard propellant. The orbital maneuvering system (e.g., nuclear or solar-powered system of electromagnetic thrusters) allows the space station or asteroid to compensate for the delta-V’s so imparted, and adjust its orbit to achieve desirable parameters.

An object in an elliptical solar orbit tangent to Earth orbit at perihelion, but with semi-major

axis ~ 1.66 a.u., has a natural orbital period of roughly 25.6 months – the interval between Mars mission opportunities from Earth. If the semi-major axis of the orbit can be rotated appropriately about the Sun every orbit, through the use of electromagnetic propulsion an gravitational assists from the Moon and Mars, etc., good rendezvous opportunities will be provided every orbit.

The railgun, combined with gravitational assists from Mars and aerobraking, and perhaps some residual delta-V provided by traditional means, offers an efficient and economic rendezvous technique for spacecraft departing the space station or asteroid for Mars.

Track 5E 2:00

Reducing Risk and Complexity of Rover and Robotic Operations on Mars

Russell R Mellon

Director of Research and Development

Equinox Interscience, Inc

6420 S. Quebec St., Ste E

Englewood, CO 80111

anchorrt@performancesw.com

The presentation offers a perspective on utilization of the Mars Raptor Reconnaissance System and its variations to reduce the risk and complexity of rover and robotic operations on Mars.

The presentation will enhance the participants understanding of issues and concerns regarding robotic and rover operations on Mars. We will present a mission risk mitigation approach to the current Lander/Rover operations for improving probability of success. This approach utilizes the Mars Raptor system that allows a least time/safest path-vs-minimum distance path for rover/robot operations. The system is a reconnaissance approach with compact, lightweight optical sensors, CCD focal planes, and High-Density Interconnect (HDI) electronics.

The presentation content will consider:

  1. Rover/Robot requirements and how they play with lander/orbiter requirements
  2. Reconnaissance methods
  3. Reconnaissance deployment scenarios
  4. Compact optical designs
  5. Bird/Nest data exchanges
  6. Data utilization and operations decision making

Track 5E 2:30

A Mission to Mars With Two Chimpanzees Before the First Human Mission to that Planet

Antonio de Morais (IF-USP University, Brazil)

macca@cbpfsu1.cat.cbpf.br

The focus of the first human expedition to outside the Earth-Moon system is In the exploration of the Moon robot spacecraft were sent before brave persons were there. In the same way robot spacecraft are being sent to Mars before the first humans get at the Red Planet. People will train in the International Space Station, and there are plans of returning to the Moon for more training to a voyage to Mars. This conquest of Mars will be a base stone in the evolution of Mankind.

But, the minimum distance between Earth and Mars is 150 times greater than the distance Earth-Moon. This enormous distance sets great difficulties to a human mission to Mars. The Martian environment has nothing to do with the lunar and terrestrial environments; not to say the fact that if a Moon

manned mission have a problem, it is still be possible to save the crew in few days, while if a manned mission be in the middle of the journey to Mars, and a problem occur, it will not be possible to save the crew. Maximum safety to the crew is a fundamental matter.

This era of Mars exploration is analogous to the days when humans were trying to orbit alone the Earth. So, I propose that, after the last robotic mission to return samples of Mars back to Earth, and before the first human journey to the Red Planet, there is the sending of two chimpanzees (male and female) to Mars returning them back to Earth, inside a semi-robotic, Earth-controlled, adapted, operational spacecraft. This mission would test completely the technology of the spacecraft (with living beings inside, breathing, feeding and performing tasks), and of the life-support systems (to the human crews) in the real Martian environment, and to test the use of astronaut life-supporting suits in real soil and atmospheric extreme weather conditions, during a long time.

The conquest of Mars is known to have been full of problems and accidents (73 percent of the total missions to Mars failed), mentioning the accident with the very expensive and complex Mars Observer spacecraft. And all these missions are automated, very far from the complexity of a manned trip to Mars. And in the history of manned space exploration, there were several accidents, mentioning the following: Vostok (Mr. Vladmir Komarov), Apollo I, Apollo XIII, Space Shuttle Challenger, MIR; and problems with practically all manned missions (and all these missions are close to Earth). A manned mission to Mars is greatly expensive and it’s objective is not only to walk on another planet, but fundamentally to develop new technologies for human use and to increase scientific knowledge the maximum as possible.

I surmise that an astronaut would like to be the first at Mars, but I also surmise the astronaut would like to know that his/her mission to Mars had the maximum study and best test for the security of functioning of the spacecraft technology and of the life-support systems, during the real cruise to (and back from) Mars, and at the real Martian environment. For that task, the two chimpanzees (male and female) would be used to live with each other, and both used to practice the operational maneuvers for the Mars mission, since their infancy. When both chimpanzees arrive at their adult phase, they would be more intensively trained and live inside an operational replica of the spacecraft (on the ground), exiting this ambient to walk (using easy-dressing spacesuits with a tensile flexing string firmly attached to the suits) around a Martian scenario, performing tasks such as getting stones on the scenario’s ground. The chimpanzees would train inside the real International Space Station inside a module (without humans). In the replica at the scenario and in the real ISS, the two would feed on vitamin fortified, colorful, tasteful, somewhat difficult to get (chimpanzees like to go for it) rich-nutrient pills, and drink water and juices, for months. Also, they would exercise, and perform several tasks, and have recreation hours (for example drawing colors on a digital screen with digital pens, playing with toys, etc.) during the tests of months, and during the real mission to Mars. They would have sensors implanted inside their bodies for the taking (via radio) of the necessary medical data (the couple would take out the sensors if put on the skin). The chimpanzees would be passed through a surgery to not be able to exist pregnancy (a factor of great complication for this mission to Mars with the chimpanzees - if the two return alive from the voyage to Mars). This mission with chimpanzees to Mars can sound funny but it is not funny the cost of human lives in a first manned mission to Mars, also reflecting on the entire manned space exploration program.

Chimpanzees have bones and cardiovascular systems stronger than man’s; if they could not resist an Earth-Mars-Earth voyage, it will be needed more studies and tests for a human visit to the Red Planet. In the history of space exploration, there are two principal characteristics: the unexpected important technological and scientific discoveries, and the unexpected of accidents and problems (usually big ones) in the missions. Resuming: the unexpected. It is fundamental to be well prepared to do it. It is because I propose that firstly be sent two chimpanzees (male and female) to planet Mars before humans get there.

Track 5E 3:00

Modeling and Simulation of a Pressure Feed System Rocket Engine to Use in Mars Ascent Vehicle (MAV)

Jos Miraglia - Engenheiro Quømico - Mestre em Propuls_o ( ITA 1994)

ITA - (Technical Institute of Aeronautics) Brazil

miraglia@mandic.com.br

The future explorations manned to the planet Mars can use the production in-situ of propellant CH4 / LOX.

This paper presents the mathematical modeling and the computational simulation of a rocket engine using as propellant CH4 / LOX, and of the launch of a Mars Ascent Vehicle (MAV) using this engine as propulsion system.

The proposed engine is a pressure feed system type, due its simplicity and operational robustness.

The motor is divided in the following elements:

Reservoir of Methane;

Reservoir of Oxygen;

Reservoir of gas pressurizer (Helium);

Tubes and accessories (valves, filters, hole plates);

Combustion chamber;

Nozzle;

The thermo/chemical and physical/chemistries properties of the propellants in subject are presented.

The engine and the launch of MAV will be simulate with the use of programs computations developed by the author.

The numeric results of the simulation of the rocket engine are presented in the graphics form.

Thrust x Time;

CH4 flow rate x Time;

LOX flow rate x Time;

O/F x Time;

Medium temperature of the combustion chamber x Time

The results of this simulation are used as parameters for the simulation of the launch of Mars Ascent Vehicle.

This simulation will be made with the use of program computations developed by the author.

The numeric result of the launch is presented in the graphics form.

Altitude x Time;

Reach horizontal x Time;

Speed x Time;

Acceleration x Time;

Track 5E 3:30

Case for an ISRU Refinery

Kelly R. McMillen

Boulder Center for Science and Policy

During the early phases of human Mars exploration, in situ resource utilization (ISRU) will lower costs, expand capabilities, and serve as an enabling technology for establishing permanent colonies. Martian atmospheric resources can be used to provide consumables such as fuel, oxidant, breathable air, and water that are critical for early human missions. Martian atmospheric carbon dioxide and imported hydrogen can be used, for example, as feedstock for the catalytic production of oxygen, methane, methanol, and other propellants and water (Zubrin, 1991, 1996, 1997, 1998, Zubrin, Meyer, McMillen 1998, Meyer 1981).

These processes utilize catalytic reactors containing small amounts of iron, nickel and other suitable catalysts, plus gas selective membranes, electrolysis, and other easily implemented gas separation techniques. Waste carbon monoxide from carbon dioxide reduction processes together with hydrogen can be combined to produce other liquid and gaseous fuels and chemical compounds. Excess heat from an exothermic Sabatier reaction can be diverted to minimize heat requirements in endothermic processes such as the reverse water-gas shift reaction. Thus valuable synergies can be realized by integrating various processes. Oxygen and fuel production processes can be combined so the thermal and material wastes of one process can be utilized by the other thus forming a unique Martian "chemical refinery" that features internal hydrogen recycling and production of a purified carbon monoxide intermediate by-product. Turbines can also be used to recover mechanical energy from high-pressure waste gas and systems can share common hardware and feedstock systems. Thus feedstock, power, heat and mechanical energy are utilized efficiently and conserved in the design of these robust Martian atmospheric refineries whose technologies may also find applications in industrial waste utilization technology on Earth.

Track 5E 4:00

The Vaults of Mars: Architecture for a Mars Settlement

Bruce MacKenzie

Boston, MA

Track 5E 4:30

Open

Closing Plenary 5:00

Plenary Panel E

Onward to Mars!

Members of the Steering Committee