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Performance of a 10 deg conical plug nozzle using a turbojet gas generatorInternal performance data for conical plug nozzle of turbojet gas engine
Document ID
19690011401
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Huntley, S. C. (NASA Lewis Research Center Cleveland, OH, United States)
Samanich, N. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52570
Report Number: NASA-TM-X-52570
Accession Number
69N20763
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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