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Scramjet analysis, testingA survey of supersonic combustion ramjet (scramjet) engine development in the US covers development of this unique engine cycle from its inception in the early 1960's through the various programs currently being pursued and, in some instances, describing the future direction of the programs. These include developmental efforts supported by the US Navy, NASA, and US Air Force. Results of inlet, combustor, and nozzle component tests, free-jet engine tests, analytical techniques developed to analyze and predict component and engine performance, and flight-weight hardware development are presented. These results show that efficient scramjet propulsion is attainable in a variety of flight configurations with a variety of fuels. Since the scramjet is the most efficient engine cycle for hypersonic flight within the atmosphere, it should be given serious consideration in future propulsion schemes.
Document ID
19920012289
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leingang, J. L.
(Wright Research Development Center Wright-Patterson AFB, OH, United States)
Stull, F. D.
(Wright Research Development Center Wright-Patterson AFB, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Publication Information
Publication: NASA. Lewis Research Center, Rocket-Based Combined-Cycle (RBCC) Propulsion Technology Workshop. Tutorial Session
Subject Category
Aircraft Propulsion And Power
Accession Number
92N21532
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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