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 vectorable 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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    Titel :

    Conceptual design of a STOVL fighter/attack aircraft


    Beteiligte:
    Chin, Y. T. (Autor:in)

    Erscheinungsdatum :

    01.10.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch