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Design and cooling performance of a dump- cooled rocket engineDesign and evaluation of liquid hydrogen cooled rocket engine for determining minimum satisfactory coolant flow
Document ID
19660022898
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Curley, J. K. (NASA Lewis Research Center Cleveland, OH, United States)
Masters, P. A. (NASA Lewis Research Center Cleveland, OH, United States)
Pavli, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Schwartz, R. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3532
Accession Number
66N32188
Funding Number(s)
CONTRACT_GRANT: 730-100-31-06-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ENGINE COOLANT
ROCKET ENGINE DESIGN
LIQUID HYDROGEN

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