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 integrated approach to an integrated program to achieve integrated flight propulsion control technology.


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    Titel :

    Flight propulsion control integration for V/STOL aircraft


    Beteiligte:

    Erscheinungsdatum :

    1987-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Flight Propulsion Control Integration for V/STOL Aircraft

    Mihaloew, James R. | SAE Technical Papers | 1987


    Flight/propulsion control integration for V/STOL fighter/attack aircraft

    Franklin, James A. / Stortz, Michael W. | NTRS | 1989


    Future Challenges in V/STOL Flight Propulsion Control Integration

    Mihaloew, J. / Miller, R. J. / Roth, S. P. | SAE Technical Papers | 1980


    Future challenges in V/STOL flight propulsion control integration

    Roth, S. P. / Miller, R. J. / Mihaloew, J. | NTRS | 1980