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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SYSTEME DE TRANSPORT HYPERSONIQUE


    Weitere Titelangaben:

    HYPERSONIC TRANSPORT SYSTEM
    HYPERSCHALLTRANSPORTSYSTEM


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

    Erscheinungsdatum :

    07.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64G Raumfahrt , COSMONAUTICS



    Système de transport hypersonique

    PRAMPOLINI MARCO / DUTHEIL JEAN-PHILIPPE / BOUE YOAN | Europäisches Patentamt | 2024

    Freier Zugriff

    SYSTEME DE TRANSPORT HYPERSONIQUE

    PRAMPOLINI MARCO / DUTHEIL JEAN-PHILIPPE / BOUE YOAN | Europäisches Patentamt | 2022

    Freier Zugriff