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Experimental investigation of hot-gas side heat-transfer rates for a hydrogen-oxygen rocketHot-gas side heat-transfer rates for liquid oxygen and hydrogen propellant rocket nozzle
Document ID
19650016811
Document Type
Other - NASA Technical Note (TN)
Authors
Jones, W. L. (NASA Lewis Research Center Cleveland, OH, United States)
Quentmeyer, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Schacht, R. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-2832
Accession Number
65N26412
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET NOZZLE
LIQUID PROPELLANT ROCKET ENGINE
HEAT TRANSFER
HOT GAS SYSTEM

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