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Investigation of Mars In-Situ Propellant Production
ISSN: 0148-7191, e-ISSN: 2688-3627
Published July 01, 1997 by SAE International in United States
Annotation ability available
In-situ production of oxygen and methane for utilization as a return propellant from Mars for both sample-return and manned missions is currently being developed by NASA in cooperation with major aerospace companies. Various technologies are being evaluated using computer modeling and analysis at the system level.
An integrated system that processes the carbon dioxide in the Mars atmosphere to produce liquid propellants has been analyzed. The system is based on the Sabatier reaction that utilizes carbon dioxide and hydrogen to produce methane and water. The water is then electrolyzed to produce hydrogen and oxygen. While the hydrogen is recycled, the propellant gases are liquefied and stored for later use. The process model considers the surface conditions on Mars (temperature, pressure, composition), energy usage, and thermal integration effects on the overall system weight and size. Current mission scenarios require a system that will produce 0.7 kg of propellant a day for 500 days.
This paper will outline a baseline system for a return propellant production plant, including power requirements and weight estimates, as well as identify key technological improvements required to develop a viable and robust system.
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CitationReddig, M. and MacKnight, A., "Investigation of Mars In-Situ Propellant Production," SAE Technical Paper 972496, 1997, https://doi.org/10.4271/972496.
- Kaplan, D.I. “Mars Sample Return Using In-Situ Propellant Production” Space 96 Conference Albuquerque, NM June 4 1996
- Trusch, R.B. Thompson C.D. Brose H.F. Atmosphere Revitalization in the Space Station Prototype ASME Environmental Control & Life Support Systems Conference San Francisco, CA August 1972
- Lunde, P.J. Kester F.L. Rates of Methanation from Carbon Dioxide and Hydrogen Over a Ruthenium Catalyst Journal of Catalysis 30 423 429 1973
- Verostko, C.E. Forsythe R.K. A Study of the Sabatier-Methanation Reaction Intersociety Conference on Environmental Systems Seattle, WA 1974
- Cusick, R.J. Space Station Prototype Sabatier Reactor Design Verification Testing Intersociety Conference on Environmental Systems Seattle, WA 1974
- Lunde, P.J. Kester F.L. Carbon Dioxide Methanation on a Ruthenium Catalyst Ind. Eng. Chem., Process Des. Develop. 13 1 1974
- Lunde, P.J. Modeling Simulation, and Operation of a Sabatier Reactor Ind. Eng. Chem., Process Des. Develop. 13 3 1974
- Naumov, V.A. Gavrilov L.I. Determination of the Kinetic Parameters of the Sabatier Reaction over Nickel Catalyst from the Critical Ignition Conditions KILLEGIBLEet. Catal. 20 1306 1308 1979
- Birbara, P.J. Sribnik F. Development of an Improved Sabatier Reactor 9 th Intersociety Conference on Environmental Systems San Francisco, CA 1979
- Forsythe, R.K. Verostko C.E. Cusick R.J. Blakely R.L. A Study of Sabatier Reactor Operation in Zero “G” 14 th Intersociety Conference on Environmental Systems San Diego, CA 1984
- Noyes, G.P. Cusick R.J. Initial Development and Performance Evaluation of a Process for Formation of Dense Carbon by Pyrolysis of Methane 15 th Intersociety Conference on Environmental Systems San Francisco, CA 1985
- Otsuji, K. Sawada T. Satou S Minemoto M. Concept Study of Regenerable Carbon Dioxide Removal and Oxygen Recovery System for the Space Station International Symposium on Space Technology and Science Tokyo, Japan 1986
- Sargent, D.H. System Level Water Balance for Space Station Freedom 20 th Intersociety Conference on Environmental Systems Williamsburg, Virginia 1990
- Strumpf, H.J. Chin C.Y. Sabatier Carbon Dioxide Reduction System for Long-Duration Manned Space Application International Conference on Environmental Systems San Francisco, CA 1991
- Zubrin, R. Price S. O'Handley D. An End-to-End Demonstration of a Full Scale Mars In-Situ Propellant Production Unit 46 th International Astronautical Congress Oslo, Norway October 2-6 1995
- Wright, R.M. Ruder J.M. Dunn V.B. Hwang K.C. “Development of Design Information for Molecular-Sieve Type Regenerative CO2 Removal Systems,” NASA Report CR-2277 AES Report 72-8417 1972
- Chang, C.H. Rousseau J. “Space Station Molecular Sieve Development,” NASA Contract NAS8-36424, Marshall Space Flight Center, Final Report 1986
- Kay, R.J. Tom R. “Two-Bed Carbon Molecular Sieve Carbon Dioxide Removal System Feasibility Testing,” ICES Paper 880993 1988
- Rose, S.K. Daviand S. Dams R.A.J. Tan G. “CO2 Removal by Hydrophobic Molecular Sieves,” ICES Paper 932271 1993
- McElroy, J.F. Molter T.M. Roy R.J. SPE Water Electrolyzers for Closed Environment Life Support 21 st International Conference on Environmental Systems San Francisco, CA 1991
- McElroy, J.F. SPE Regenerative Hydrogen/Oxygen Fuel Cells for Space and Marine Applications Fuel Cell Seminar 1990
- Scott, R.B. Denton W.H. Nicholls C.M. “Technology and Uses of Liquid Hydrogen” Macmillan Company New York 1964
- Preparation of Hydrophobic Molecular Sieve 1990