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Experiments with hydrogen and oxygen in regenerative engines at chamber pressures from 100 to 300 pounds per square inch absoluteDesign of lightweight regeneratively cooled hydrogen-oxygen thrust chamber
Document ID
19660024054
Document Type
Technical Memorandum (TM)
Authors
Bartoo, E. R. (NASA Lewis Research Center Cleveland, OH, United States)
Rollbuhler, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Tomazic, W. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1960
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-253
Accession Number
66N33344
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REGENERATIVE COOLING
LIQUID HYDROGEN
LIQUID OXYGEN /LOX/
COMBUSTION CHAMBER

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