The invention discloses an integrated rail type cube satellite launching device used to carry or launch a single or multiple cube satellites. The integrated rail type cube satellite launching device mainly comprises a rectangular frame, an unlocking mechanism, a spring mechanism and the like, wherein the rectangular frame is mainly formed by connecting a cabin door, a baffle, a bottom plate, side plates, an upper cover plate, a rear cover plate and the like through threads. An upper plate, a lower plate, a left plate and a right plate are symmetrically distributed along the long axis and form a thin boss, and each two of the upper plate, the lower plate, the left plate and the right plate form an integrated type rail used as a satellite slide rail. Components of a sucker magnet and the like are used as an unlocking mechanism. A spring mechanism comprises a push plate and a press spring. The integrated rail type cube satellite launching device is strong in universality and low in cost, can guarantee transportation safety and launching reliability of the cube satellites, can prevent the cube satellites from shifting during the transportation process, prevents the cabin door from striking a revolving platform or reversely revolving during the opening process, and provides push plate ejection prevention measures and the like.


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    Titel :

    Integrated rail type cube satellite launching device


    Beteiligte:
    SHEN NA (Autor:in) / BAO JIAQIAN (Autor:in) / ZHANG XIANGJIN (Autor:in) / LIAO QIAOSHENG (Autor:in) / WU ZHILIANG (Autor:in)

    Erscheinungsdatum :

    22.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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