Crew systems and architectural considerations for first lunar surface return missions

Details Crew systems and architectural considerations for first lunar surface return missions Crew systems and architectural considerations for first lunar surface return missions

Aug 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992wadc.iafcz....w&link_type=abstract

IAF, International Astronautical Congress, 43rd, Washington, Aug. 28-Sept. 5, 1992. 14 p.

Astronomy and Astrophysics

Astronomy

Lunar Bases, Lunar Surface, Pressurized Cabins, Space Habitats, Spacecrews, Escape Rockets, Extravehicular Activity, Life Support Systems, Lunar Landing, Mission Planning

Scientific paper

The design requirements for the habitability of the pressurized volumes of a typical first manned lander are presented. Attention is given to providing dual habitation/exploration services (EVA/IVA), supporting the separation of the surface/flight functions, allowing growth potential based on site characteristics, and in situ resources utilization. Lunar lander conceptual diagrams are provided for the basic system architecture, automatic cargo delivery, the piloted crew module, and the pressurized volumes.

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