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NASP X-30 Propulsion technology statusThe performance goals of the NASP program require an aero-propulsion system with a high effective specific impulse. In order to achieve these goals, the high potential performance of air-breathing engines must be achieved over a very wide Mach number operating range. This, in turn, demands high component performance and involves many important technical issues which must be resolved. Scramjet Propulsion Technology is divided into five major areas: (1) inlets, (2) combustors, (3) nozzles, (4) component integration, and (5) test facilities. A status report covering the five areas is presented.
Document ID
19920012291
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Powell, William E.
(National Aero-Space Plane Joint Program Office 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
92N21534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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