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Mars hardware

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Martian Outpost

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Abstract

The hardware described in this chapter is based on the architecture proposed by SpaceWorks Engineering Inc. (SEI) [6]. The SEI architecture (see Chapter 3) is similar to NASA’s Constellation Design Reference Mission (DRM) and assumes a manned Mars mission will utilize the major elements of NASA’s Constellation development effort including a new family of all-chemical launch vehicles, flight components, ground services and no in-situ resource utilization (ISRU).

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References

  1. Advanced Transportation System Studies Technical Area 2 (TA-2). Heavy Lift Launch Vehicle Development Contract. NAS8-39208. DR 4. Final Report. Prepared by Lockheed Martin Missiles & Space for the Launch Systems Concepts Office of the George C. Marshall Space Flight Center. (July 1995).

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  2. Constellation Architecture Requirements Document. NASA CxP 70000. Baseline. December 21, 2006.

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  3. Exploration Systems Architecture Study. Final Report. NASA-TM-2005-214062. (November 2005).

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  4. NASA. Man-Systems Integration Standards. NASA STD-3000. Houston, TX: NASA Johnson Space Center. 1995.

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  5. Simonsen, L.C., and Nealy, J.E. Mars Surface Radiation Exposure for Solar Maximum Conditions and 1989 Solar Proton Events. NASA TP-3300, 1993.

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  6. St. Germain, B.; Olds, J.R.; Bradford, J.; Charania, A.C.; DePasquale, D.; Schaffer, M.; Wallace, J. Utilizing Lunar Architecture Transportation Elements for Mars Exploration. SpaceWorks Engineering, Inc. (SEI), Atlanta, GA, 33075. 2007.

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© 2009 Praxis Publishing Ltd.

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Seedhouse, E. (2009). Mars hardware. In: Martian Outpost. Springer Praxis Books. Praxis. https://doi.org/10.1007/978-0-387-98191-8_6

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