The application of SP-100 technology in a lunar surface power system

Details The application of SP-100 technology in a lunar surface power system The application of SP-100 technology in a lunar surface power system

Sep 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991asei.conf.....u&link_type=abstract

AIAA, NASA, and OAI, Conference on Advanced SEI Technologies, Cleveland, OH, Sept. 4-6, 1991. 8 p.

Physics

Design Analysis, Lunar Surface, Space Power Reactors, Systems Engineering, Lunar Environment, Propulsion System Configurations, Structural Design, Technologies

Scientific paper

Consideration is given to a conceptual design study addressing the application of the SP-100 space reactor power system technology to a lunar surface power system (LSPS). Data obtained demonstrate that the SP-100 technology can be readily adapted to the lunar environment to meet the load demands of the lunar outpost. Particular attention is given to the conceptual design for a 100 kWe LSPS based on the technology and design for the orbital SP-100 generic flight system and an overall power system architecture based on the sequential emplacement of four 50 kWe thermoelectric LSPS units and two 375 kWe LSPS units.

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