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Apollo experience report: Lunar module electrical power subsystemThe design and development of the electrical power subsystem for the lunar module are discussed. The initial requirements, the concepts used to design the subsystem, and the testing program are explained. Specific problems and the modifications or compromises (or both) imposed for resolution are detailed. The flight performance of the subsystem is described, and recommendations pertaining to power specifications for future space applications are made.
Document ID
19720025198
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Campos, A. B.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
MSC-S-337
NASA-TN-D-6977
Accession Number
72N32848
Funding Number(s)
PROJECT: RTOP 914-13-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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