A rocket catapult assembly for an ejection seat may comprise a motor assembly including a proximal end and a distal end, an outlet tube coupled to the distal end, and a valve coupled to the outlet tube. The valve may be configured to vary an operating pressure based on an occupant's weight. The valve may be in a closed configuration, on open configuration, or a partially open configuration during ejection of the ejection seat.


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    Titel :

    Variable thrust catapult


    Beteiligte:
    WHELAN PATRICK (Autor:in) / SALOIS MATTHEW D (Autor:in) / BENJAMIN JEFF (Autor:in) / MUELLER KEVIN J (Autor:in)

    Erscheinungsdatum :

    08.02.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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