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Evaluation of speech suppression concepts in a 20,000 pound thrust hydrogen oxygen rocketStability characteristics of screech suppression concepts in hydrogen-oxygen rocket
Document ID
19670025429
Document Type
Technical Memorandum (TM)
Authors
Hannum, N. P. (NASA Lewis Research Center Cleveland, OH, United States)
Russell, L. M. (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
August 1, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-1435
Accession Number
67N34758
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ACOUSTIC STABILITY
HYDROX ENGINE
NOISE SUPPRESSOR

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