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Dynamic-model investigation of some landings and slideouts of a recoverable boosterLanding impact and slideout stability characteristics of recoverable booster
Document ID
19660024160
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Thompson, W. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-3413
Report Number: NASA-TN-D-3413
Accession Number
66N33450
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LAUNCH VEHICLE
LANDING SYSTEM
STABILITY TEST
BOOSTER RECOVERY

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