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Hypersonic research engine/aerothermodynamic integration model: Experimental results. Volume 3: Mach 7 component integration and performanceThe NASA Hypersonic Research Engine Project was undertaken to design, develop, and construct a hypersonic research ramjet engine for high performance and to flight test the developed concept on the X-15-2A airplane over the speed range from Mach 3 to 8. Computer program results are presented here for the Mach 7 component integration and performance tests.
Document ID
19760016172
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Andrews, E. H., Jr. (NASA Langley Research Center Hampton, VA, United States)
Mackley, E. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-72823
Report Number: NASA-TM-X-72823
Accession Number
76N23260
Funding Number(s)
PROJECT: RTOP 505-05-41-03
CONTRACT_GRANT: NAS1-6666
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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