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Experimental heat-transfer results for cryogenic hydrogen flowing in tubes at subcritical and supercritical pressures to 800 pounds per square inch absoluteCryogenic para hydrogen heat transfer data at near critical pressures and temperatures for advanced propulsion system coolant
Document ID
19660011645
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Friedman, R. (NASA Lewis Research Center Cleveland, OH, United States)
Graham, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Hendricks, R. C. (NASA Lewis Research Center Cleveland, OH, United States)
Hsu, Y. Y. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-3095
Accession Number
66N20934
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CRITICAL PRESSURE
CRYOGENIC FLUID
PARA HYDROGEN
HEAT TRANSFER
PROPULSION SYSTEM

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