Short takeoff vertical landing (STOVL) aircraft offer unique basing and operational advantages to improve the capabilities of military forces in future warfare. To develop a STOVL fighter design with supersonic capability requires the integration of an advanced propulsion system into the airframe design. A promising propulsion system for supersonic STOVL application is the relatively new Hybrid Fan Vectored Thrust (HFVT) concept. This advanced Tandem Fan concept incorporates a dual-cycle engine with front and rear fully vectorabie nozzles of the three-poster type, to provide the required performance. In this paper, the HFVT STOVL design integration approaches for a conceptual fighter/attack aircraft, as well as some features of the resulting design, will be presented.


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    Title :

    Conceptual Design of a STOVL Fighter/Attack Aircraft


    Additional title:

    Sae Technical Papers


    Contributors:
    Chin, Y.T. (author)

    Conference:

    Aerospace Technology Conference and Exposition ; 1988



    Publication date :

    1988-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English