Lunar lander and return propulsion system trade study - Methodology with results

Details Lunar lander and return propulsion system trade study - Methodology with results Lunar lander and return propulsion system trade study - Methodology with results

Jun 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993jpmc.confsx...m&link_type=abstract

AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit, 29th, Monterey, CA, June 28-30, 1993, 14 p.

Statistics

Methodology

Liquid Propellant Rocket Engines, Lunar Landing, Methodology, Propulsion System Configurations, Return To Earth Space Flight, Liquid Hydrogen, Liquid Oxygen, Methylhydrazine, Nasa Space Programs, Nitrogen Tetroxide

Scientific paper

A trade study was initiated at the NASA/Johnson Space Center in May of 1992 to develop and evaluate main propulsion system alternative configurations for the First Lunar Outpost (FLO) lander and return vehicles. This paper outlines the trade methodology utilized in the FLO vehicle study. Emphasis is placed on the trade attributes, selection criteria, and evaluation process established to perform the comprehensive analysis required to rank the diverse alternative vehicle configurations considered. The use of sensitivity analyses to determine the relative importance of each attribute and selection criteria on the trade results is also presented. Lastly, the paper discusses FLO vehicle configuration recommendations and general vehicle design conclusions which can be drawn from the trade study results.

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