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The effect of several injector face baffle configurations on screech in a 20,000-pound thrust hydrogen-oxygen rocketEffects of injector face baffle configurations on screech in hydrogen-oxygen rocket engine
Document ID
19670002005
Document Type
Technical Memorandum (TM)
Authors
Hannum, N. P. (NASA Lewis Research Center Cleveland, OH, United States)
Scott, H. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52251
Accession Number
67N11334
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INJECTOR
LOX-HYDROGEN ENGINE
ACOUSTICS
BAFFLE

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