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Full scale tests of a short length, double annular ram induction turbojet combustor for supersonic flightPerformance tests and characteristics of short length, double annular ram induction turbojet combustion chambers for supersonic flight
Document ID
19710010816
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Perkins, P. J. (NASA Lewis Research Center Cleveland, OH, United States)
Schultz, D. F. (NASA Lewis Research Center Cleveland, OH, United States)
Wear, J. D. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-6254
E-5899
Report Number: NASA-TN-D-6254
Report Number: E-5899
Accession Number
71N20291
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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