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A mathematical procedure for predicting the touchdown dynamics of a soft-landing vehicleMathematical simulation of touchdown characteristics of soft landing spacecraft
Document ID
19710007293
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Doiron, H. H. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Zupp, G. A., Jr. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
MSC-5-241
NASA-TN-D-7045
Accession Number
71N16768
Funding Number(s)
CONTRACT_GRANT: 914-50-20-89-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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