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A resonance-tube igniter for hydrogen-oxygen rocket enginesResonance-tube igniter for hydrogen-oxygen rocket engines
Document ID
19670030753
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Conrad, E. W. (NASA Lewis Research Center Cleveland, OH, United States)
Pavli, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-1460
Report Number: NASA-TM-X-1460
Accession Number
67N40082
Funding Number(s)
CONTRACT_GRANT: 128-31-06-05-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYDROX ENGINE
IGNITER
RESONANT CAVITY

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