The invention discloses an on-orbit transfer device. The on-orbit transfer device comprises a first body, a transferred apparatus and a second body; in an initial state, the transferred apparatus is mounted in the first body; after on-orbit transfer, the transferred apparatus is installed in the second body. The on-orbit transfer device is simple and reliable in structure, can counteract a counterforce borne by the transferred apparatus during disassembly and assembly, and can be guided and locked during installation.

    本发明公开了一种在轨转移装置,包括:第一本体、被转移装置和第二本体;初始状态时,被转移装置安装于第一本体;在轨转移后,被转移装置安装于第二本体。该在轨转移装置,结构简单、可靠,拆装时可抵消被转移装置所受的反力,安装时可导向锁紧。


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    Titel :

    On-orbit transfer device


    Weitere Titelangaben:

    一种在轨转移装置


    Beteiligte:
    HUO JIE (Autor:in) / XIAN KUICHENG (Autor:in) / GU JUEHUA (Autor:in) / YIN AIPING (Autor:in) / FU QINGSHAN (Autor:in) / CHENG LEI (Autor:in) / NI XIAOFENG (Autor:in) / WANG ZHIYI (Autor:in)

    Erscheinungsdatum :

    2020-06-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS