A hypersonic vehicle includes a body; a first engine secured to the body, the first engine is configured to create forward thrust at a first flight regime; a second engine secured to the body, the second engine is configured to create forward thrust at a second flight regime; and the hypersonic vehicle transitions between the first engine and the second engine during the first flight regime and the second flight regime.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYPERSONIC VEHICLE USING SCRAMJET


    Beteiligte:

    Erscheinungsdatum :

    2019-08-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke




    Hypersonic Research Vehicle to Develop Scramjet Engines

    G. M. Gregorek / R. L. Reuss | NTIS | 1990


    Simulation of hypersonic scramjet exhaust

    Oman, R. A. / Foreman, K. M. / Leng, J. et al. | NTRS | 1975


    Airframe/Scramjet Integrated Design of Hypersonic Cruise Vehicle

    Jing, Che / Shuo, Tang / Bingnan, Kang | AIAA | 2007


    Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle

    Pezzella, Giuseppe / Marini, Marco / Cicala, Marco et al. | AIAA | 2014