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Command module/service module reaction control subsystem assessmentDetailed review of component failure histories, qualification adequacy, manufacturing flow, checkout requirements and flow, ground support equipment interfaces, subsystem interface verification, protective devices, and component design did not reveal major weaknesses in the command service module (CSM) reaction control system (RCS). No changes to the CSM RCS were recommended. The assessment reaffirmed the adequacy of the CSM RCS for future Apollo missions.
Document ID
19720023208
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Weary, D. P.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-68578
MSC-03432
Report Number: NASA-TM-X-68578
Report Number: MSC-03432
Accession Number
72N30858
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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