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Apollo command module land impact testsFull-scale-model and actual spacecraft were impact tested to define the emergency land-landing capability of the Apollo command module. Structural accelerations and strains were recorded on analog instrumentation, and a summary to these data is included. The landing kinematics were obtained from high-speed photography. Photographs of the structural damage caused during the tests are included. Even though extensive damage can be expected, the crew will receive nothing more than minor injuries during the majority of the probable landing conditions.
Document ID
19720025207
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mccullough, J. E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Lands, J. F., Jr.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
MSC-S-301
NASA-TN-D-6979
Report Number: MSC-S-301
Report Number: NASA-TN-D-6979
Accession Number
72N32857
Funding Number(s)
PROJECT: RTOP 914-50-20-17-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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