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Survey of supersonic combustion ramjet research at LangleyThe Hypersonic Propulsion Branch at NASA Langley Research Center has maintained an active research program in supersonic combustion ramjet (scramjet) and high speed ramjet propulsion since the 1960s. The focus for this research has centered on propulsion for manned reuseable vehicles with cryogenic hydrogen fuel. This paper presents some highlights of this research. The design philosophy of the Langley fixed-geometry airframe-integrated modular scramjet is discussed. The component development and research programs that have supported the successful demonstration of the engine concept using subscale engine module hardware is reviewed and a brief summary of the engine tests presented. An extensive bibliography of research supported by the Langley program is also included.
Document ID
19860052341
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Northam, G. B.
(NASA Langley Research Center Hampton, VA, United States)
Anderson, G. Y.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 86-0159
Accession Number
86A37079
Distribution Limits
Public
Copyright
Other

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