Three propulsion systems for a Mach 2 STOVL fighter were compared. The three propulsion systems are: (1) turbine bypass engine with a turbocompressor used for STOVL only; (2) turbine bypass engine with a turbocompressor for both STOVL and thrust during forward flight; and (3) mixed flow afterburning turbofan with a remote burner lift system. In the first system, the main engines have afterburners and the turbocompressors use after burning during STOVL. In the second system, the turbine bypass engines are dry and the turbocompressors have afterburners. The mission used in the study is a deck launched intercept mission. It is indicated that large improvements in combat time are possible when the turbocompressors are used for both left and thrust for forward flight.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Supersonic STOVL Aircraft with Turbine Bypass/Turbo-Compressor Engines


    Beteiligte:
    L. C. Franciscus (Autor:in) / R. W. Luidens (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Supersonic STOVL aircraft with turbine bypass/turbo-compressor engines

    Franciscus, L. C. / Luidens, R. W. | NTRS | 1984



    Supersonic STOVL aircraft with turbine bypass/turbo-compressor engines

    Franciscus, L. C. / Luidens, R. W. | NTRS | 1984


    Supersonic STOVL research aircraft

    Wilson, S. B., III / Kidwell, G. H., Jr. / Turney, G. E. et al. | NTRS | 1982


    Supersonic STOVL Research Aircraft

    Rogers, Al / Turney, George E. / Kidwell, George H. et al. | SAE Technical Papers | 1982