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EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER RATES IN ROCKET THRUST CHAMBERSAnalysis of heat transfer in rocket engine thrust chambers that use convergent-divergent nozzles
Document ID
19630017687
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Harper, E. Y.
Witte, A. B.
Date Acquired
August 1, 2013
Publication Date
February 1, 1963
Subject Category
Geophysics
Accession Number
63A13746
Distribution Limits
Public
Copyright
Other
Keywords
ROCKET ENGINE
THRUST CHAMBER
HEAT TRANSFER

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