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Flight Propulsion Control Integration for V/STOL Aircraft National Aeronautics and Space Administration Lewis Research Center Cleveland, OH

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Mihaloew, James R., author.
Conference Name:
SAE International Powered Lift Conference and Exposition (1987-12-07 : Santa Clara, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1987
Summary:
The goal of the propulsion community is to have the enabling propulsion technologies in place to permit a low risk decision regarding the initiation of a research STOVL supersonic attack/fighter aircraft in the mid-1990's. This technology will effectively integrate, enhance, and extend the supersonic cruise. STOVL, and fighter/attack programs to enable U.S. Industry to develop a revolutionary supersonic short takeoff/vertical landing fighter/attack aircraft in the post-ATF period. The rationale, methods, and criteria used in developing a joint NASA Lewis and NASA Ames research program to develop the technology element for integrated flight-propulsion control through integrated methodologies is presented. This program, the Supersonic STOVL Integrated Flight-Propulsion Controls Program, is part of the overall NASA Lewis Supersonic STOVL Propulsion Technology Program, it uses an integrated approach to an integrated program to achieve integrated flight-propulsion control technology
Notes:
Vendor supplied data
Publisher Number:
872330
Access Restriction:
Restricted for use by site license

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