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Turbojet-ramjet propulsion system for all-body hypersonic aircraftEvaluating performance characteristics of parallel turboramjet propulsion system for all-body Mach 6 hypersonic aircraft
Document ID
19710005905
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Waters, M. H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-5993
A-3668
Report Number: NASA-TN-D-5993
Report Number: A-3668
Accession Number
71N15380
Funding Number(s)
CONTRACT_GRANT: 789-50-01-01-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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