A propulsion system concept with particular application to supersonic short takeoff and vertical landing (STOVL) fighter/attack aircraft has been developed. The concept comprises a variable cycle engine, combining the advantages of a vectored thrust turbofan for takeoff, landing, and subsonic flight with those of a mixed augmented turbofan for high performance and supersonic flight. The system incorporates features and characteristics which have proved both practical and successful on the AV-8 (Harrier), and is potentially an attractive solution.


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    Titel :

    The Hybrid Fan Vectored Thrust Engine


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Ward, B. D. (Autor:in) / Penrose, C. J. (Autor:in)

    Kongress:

    Aerospace Congress and Exposition ; 1983



    Erscheinungsdatum :

    1983-10-03




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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