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WIND TUNNEL STUDIES OF BOOSTER BASE HEATINGAnalytical and experimental studies of rocket- booster base flow
Document ID
19630017281
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Beheim, M. A.
Obery, L. J.
Date Acquired
August 1, 2013
Publication Date
February 1, 1963
Subject Category
Aircraft
Accession Number
63A13340
Distribution Limits
Public
Copyright
Other
Keywords
NOZZLE FLOW
FLOW MEASUREMENT
ROCKET BOOSTER

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