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Design and analysis of a scramjet engineDesign concepts defined for the cooled-structures assembly of a hydrogen fueled, regeneratively cooled, airframe-integrated Scramjet engine are considered. Engine subsystems, in particular, the fuel subsystem associated with the operating engine are included along with the engine mounting and the interfacing with the airplane. The engine structure and thermal protection system, including the fuel injection struts are emphasized.
Document ID
19790013255
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Buchmann, O. A. (AiResearch Mfg. Co. Los Angeles, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA. Langley Res. Center Recent Advan. in Structures for Hypersonic Flight, Pt. 1
Subject Category
Structural Mechanics
Accession Number
79N21426
Funding Number(s)
CONTRACT_GRANT: NAS1-13984
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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