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SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINESSelection of thrust chamber cooling technique for liquid propelled spacecraft rocket engines
Document ID
19630007924
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Coulbert, C. D. (Marquardt Corp. Van Nuys, CA, United States)
Date Acquired
August 1, 2013
Publication Date
January 1, 1963
Subject Category
Geophysics
Report/Patent Number
AIAA PAPER-63-241
Report Number: AIAA PAPER-63-241
Accession Number
63N17800
Funding Number(s)
CONTRACT_GRANT: NAS7-103
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID PROPELLANT ROCKET ENGINE
THRUST CHAMBER
COOLING
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