Embodiments of the invention relate to a hypersonic transport system including: an aircraft which includes a hypersonic lift-to-drag ratio greater than or equal to 2.5, wherein the aircraft includes a secondary propulsion device and position sensors, and wherein the aircraft also includes a variably shaped aerodynamic surface; a main propulsion device which is removably attached to the aircraft; and a control unit which is configured to monitor the aircraft and the main propulsion device.


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    Titel :

    HYPERSONIC TRANSPORT SYSTEM


    Beteiligte:
    PRAMPOLINI MARCO (Autor:in) / DUTHEIL JEAN-PHILIPPE (Autor:in) / BOUE YOAN (Autor:in)

    Erscheinungsdatum :

    06.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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    Hypersonic transport technology

    Kirkham, F. S. / Hunt, J. L. | NTRS | 1977


    A hypersonic executive transport

    Debonis, J. / Bruns, J. / Detelich, M. et al. | NTRS | 1989