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Status of the NASA YF-12 Propulsion Research ProgramThe YF-12 research program was initiated to establish a technology base for the design of an efficient propulsion system for supersonic cruise aircraft. The major technology areas under investigation in this program are inlet design analysis, propulsion system steady-state performance, propulsion system dynamic performance, inlet and engine control systems, and airframe/propulsion system interactions. The objectives, technical approach, and status of the YF-12 propulsion program are discussed. Also discussed are the results obtained to date by the NASA Ames, Lewis, and Dryden research centers. The expected technical results and proposed future programs are also given. Propulsion system configurations are shown.
Document ID
19760012064
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Albers, J. A.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-56039
H-935
Report Number: NASA-TM-X-56039
Report Number: H-935
Accession Number
76N19152
Funding Number(s)
PROJECT: RTOP 516-51-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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