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SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINESRegenerative and radiation cooling, transpiration or film cooling, ablation and inert or endothermic heat sink, used in selecting optimum spacecraft engine thrust chamber cooling techniques
Document ID
19630023320
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Coulbert, C. D.
Date Acquired
August 1, 2013
Publication Date
June 20, 1963
Subject Category
Propellants
Report/Patent Number
AIAA PAPER 63-241
Report Number: AIAA PAPER 63-241
Accession Number
63A19379
Funding Number(s)
CONTRACT_GRANT: NAS7-103
Distribution Limits
Public
Copyright
Other
Keywords
ENGINE COOLANT
SPACECRAFT PROPULSION
COOLING SYSTEM
THRUST CHAMBER

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