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Low-speed dynamic model investigation of Apollo command module configurations in the Langley spin tunnelDynamic stability of Apollo command module with and without drogue parachutes at low subsonic speeds in spin tunnel
Document ID
19670023693
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Burk, S. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Lee, H. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-3888
Accession Number
67N33022
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMMAND MODULE
DROGUE PARACHUTE
APOLLO SPACECRAFT
DYNAMIC STABILITY

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