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Apollo experience report: Lunar module structural subsystemIn the Apollo Program, the lunar-orbit rendezvous mode was used for the lunar-landing mission. To accomplish the lunar landing, a lunar module spacecraft was built. A description of the design requirements for the structural subsystem and of the structural configuration and the method of design verification are given. A discussion is presented of several problems encountered and the corrective actions taken during the designing, manufacturing, and testing of the lunar module.
Document ID
19730010174
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Weiss, S. P.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-7084
MSC-S-345
Accession Number
73N18901
Funding Number(s)
PROJECT: RTOP 914-13-20-13-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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