Design and development of pressure-fed, sixteen-engine, bipropellant reaction control system for Apollo Lunar Module; design requirements, from which basic configuration evolved, as well as detailed system description are presented; overall development program is outlined and principal development problems and solutions are discussed; significant ground test techniques and results are summarized; highlights of system assembly and checkout are described. (31690)
Apollo Lunar Module control system
ASME Aviation Space -- Progress Prospects
ASME Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Control
1968
11 pages
Aufsatz (Konferenz)
Englisch
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The Apollo Lunar Module Reaction Control System.
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