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Apollo experience report: Spacecraft structure subsystemThe flightworthiness of the Apollo spacecraft structure was verified primarily through a rigorous, vehicle level, ground test program and flight tests. The failures and anomalies encountered during this testing were the major factors considered in determining necessary modifications to the basic design of the spacecraft structure. In this report, these failures, their causes, and their resolutions are discussed. A description of the spacecraft structure and discussions of the ground and flight test programs are presented.
Document ID
19740026226
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Smith, P. D.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1974
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-7780
JSC-S-400
Accession Number
74N34339
Funding Number(s)
PROJECT: RTOP 914-50-31-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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