Analysis of a spacecraft life support system for a Mars mission

Author:

Czupalla M,Aponte V,Chappell S,Klaus D

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. NASA Design Reference Mission (DRM) for Mars, Addendum 3.0, from the world wide web: http://exploration.jsc.nasa.gov/marsref/contents.html.

2. A. Chutjian, et al., A miniature quadrupole mass spectrometer array and GC for space flight: astronaut EVA and cabin-air monitoring, International Conference on Environmental Systems, Society for Automotive Engineers, Warrendale, PA, 2000, Paper No. 2000-01-2300.

3. J.E. Finn, K.R. Sridhar, C.P. McKay, Utilization of Martian atmosphere constituents by temperature-swing adsorption, in: R.M. Zubrin (Ed.), From Imagination to Reality: Mars Exploration Studies of the Journal of the British Interplanetary Society, Part I: Precursors and Early Piloted Missions, Vol. 91, AAS Science and Technology Series, 1997, pp. 127.

4. K.R. Sridhar, M. Gottman, R.S. Baird, AIAA 99-2413 2001 Mars in-situ oxygen production flight demonstration, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, CA, June 1999.

5. A.J. Hanford, M.K. Ewert, D.L. Henninger, 2002, Advanced Life Support Baseline Values and Assumptions Document, Reference No. CTSD-ADV-383, NASA JSC, Engineering Directorate, Crew and Thermal Systems Division.

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