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THRUST CHAMBER COOLING TECHNIQUES FOR SPACECRAFT ENGINES. VOLUME I- EVALUATION PROCEDURE AND ANALYSESLiquid propellant rocket engine - cooling system, ablation, and heat sink
Document ID
19630011163
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Batha, D. R. (Marquardt Corp. Van Nuys, CA, United States)
Campbell, J. G. (Marquardt Corp. Van Nuys, CA, United States)
Carey, M. D. (Marquardt Corp. Van Nuys, CA, United States)
Coulbert, C. D. (Marquardt Corp. Van Nuys, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 15, 1963
Subject Category
Propellants
Report/Patent Number
NASA-CR-50958
Report Number: NASA-CR-50958
Accession Number
63N21043
Funding Number(s)
CONTRACT_GRANT: NAS7-103
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COOLING SYSTEM
HEAT SINK
ABLATION
LIQUID PROPELLANT ROCKET ENGINE

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