A VTOL FLIGHT SYSTEM The present invention relates to a system of aircraft involving a fixed-wing aircraft 5 (100) and at least an external agent (199) capable of VTOL that form a momentary short / vertical takeoff and landing (STOL / VTOL) flight system when required. Embodiments of the external agent (199) include rotary-wing aircraft (200). Most Illustrative Diagram: FIG. 3(b) cv)r a-L


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    Title :

    A VTOL FLIGHT SYSTEM


    Contributors:

    Publication date :

    2021-10-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




    Proposed VTOL flight requirements

    Griffith, J.H. | Engineering Index Backfile | 1963


    VTOL IFR in-flight simulation

    Bondurant III, R.A. | Engineering Index Backfile | 1968


    Flying VTOL Flight Simulator Study

    T. Dukes / R. Gangwish | NTIS | 1960


    VTOL flight control in 1980

    DENDY, J. / TRIBKEN, E. | AIAA | 1968