Basic requirements and design considerations; propulsion system conceived for high speed VTOL aircraft by Aircraft Gas Turbine Div, General Electric, Evendale, Ohio; conventional turbojet sized so it will produce adequate cruise thrust at moderate altitudes and attractive subsonic speeds; lift fan is driven by engine which is shut down during cruise; specific convertible VTOL aircraft design.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Some thoughts on VTOL propulsion


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Kappus, P.G. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    VTOL propulsion

    Jacobson, D.H. / Hockert, C.E. | Engineering Index Backfile | 1965


    VTOL aircraft with electric propulsion

    STOBBE MARTIN / RAJPUT KRISHNA PAL / MORES SEBASTIAN | Europäisches Patentamt | 2024

    Freier Zugriff

    Propulsion spectrum for VTOL aircraft

    Richardson, D.A. | Engineering Index Backfile | 1959



    A PROPULSION SPECTRUM FOR VTOL AIRCRAFT

    RICHARDSON, D. A. | SAE Technical Papers | 1959