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Some injector element detail effects on screech in hydrogen-oxygen rocketsConcentric tube injection effect on dynamic characteristics of hydrogen-oxygen rocket
Document ID
19670030892
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Conrad, E. W. (NASA Lewis Research Center Cleveland, OH, United States)
Hannum, N. P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52363
Accession Number
67N40221
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET THRUST
TUBE
GAS INJECTION
HYDROX ENGINE

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