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Some factors influencing heat transfer to liquid-propellant rocket-thrust-chamber coolant channelsWall temperature and heat transfer patterns in liquid-propellant rocket thrust chamber coolant channels
Document ID
19660030242
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Curren, A. N.
Krueger, R. C.
Date Acquired
September 2, 2013
Publication Date
November 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3671
Report Number: NASA-TN-D-3671
Accession Number
66N39532
Funding Number(s)
CONTRACT_GRANT: 128-31-06-01-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID PROPELLANT ROCKET ENGINE
COOLING SYSTEM
HEAT TRANSFER

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