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Analytical model for determining spacecraft impact velocity and orientation relative to an impact surfaceDevelopment of analytical model for determining spacecraft impact velocity and orientation relative to impact surface for variable dynamic conditions
Document ID
19710015923
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Howes, D. B. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Whitnah, A. M. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
MSC-S-237
NASA-TN-D-6325
Accession Number
71N25399
Funding Number(s)
CONTRACT_GRANT: 914-50-11-09-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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