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Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzlesOff-design performance levels for divergent- ejector-type rocket nozzles
Document ID
19660024056
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gertsma, L. W. (NASA Lewis Research Center Cleveland, OH, United States)
Yeager, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1960
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-250
Report Number: NASA-TM-X-250
Accession Number
66N33346
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET NOZZLE
DIVERGENT NOZZLE
EJECTOR

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