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A hot gas generator for large scale supersonic combustor testingExhaust gas of hydrazine-nitrogen tetroxide rocket for simulating combustor inlet requirements of scramjet engines
Document ID
19680024882
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lezberg, E. A. (NASA Lewis Research Center Cleveland, OH, United States)
Metzler, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52433
Report Number: NASA-TM-X-52433
Meeting Information
Meeting: PROPULSION JOINT SPECIALIST CONF.
Location: CLEVELAND
Start Date: June 10, 1968
End Date: June 14, 1968
Sponsors: AIAA
Accession Number
68N34354
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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