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Effect of propellant injection velocity on screech in 20,000-pound hydrogen-oxygen rocket enginePropellant injection velocity effect on screech in 20,000 pound hydrogen-oxygen rocket engine
Document ID
19660011747
Document Type
Other - NASA Technical Note (TN)
Authors
Conrad, E. W. (NASA Lewis Research Center Cleveland, OH, United States)
Parish, H. C. (NASA Lewis Research Center Cleveland, OH, United States)
Wanhainen, J. P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3373
Accession Number
66N21036
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
ENGINE TESTING
INJECTION

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