A payload joint (10) for detachably attaching to each other two adjacent construction elements (2) in a spacecraft and/or launch vehicle, the payload joint (10) comprises two opposing clamps (11a, 11b) and two opposing flanges of the construction elements collaborating with angled surfaces of the clamps (11a, 11b). The payload joint comprises a bolt that connects the clamps (11a, 11b) and drives them towards each other when tightening the payload joint (10). The payload joint (10) further comprises a bolt cutter (101) arranged for cutting the the bolt upon activation.


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    Titel :

    PAYLOAD DISPENSER


    Weitere Titelangaben:

    NUTZDATENAUSGABE
    DISTRIBUTEUR DE CHARGE UTILE


    Beteiligte:
    ARULF ÖRJAN (Autor:in) / ÖHLIN JOHAN (Autor:in)

    Erscheinungsdatum :

    12.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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