The invention relates to the technical field of spaceflight, in particular to a tether releasing device applied to a space tether, which comprises an ejection component, the ejection component is fixedly connected with the space tether, a spool component and a brake component are sequentially and fixedly connected below the ejection component, the middle of the space tether penetrates through the spool component, and the tail end of the space tether is fixedly connected with the brake component. According to the invention, the aim of simplifying the design and compactly installing the tether releasing device can be achieved.

    本发明涉及航天技术领域,特别是涉及一种应用于空间绳系的系绳释放装置,包括弹射组件,弹射组件固接有空间绳系,弹射组件下方依次固接有线轴组件和制动组件,空间绳系中部穿过线轴组件,空间绳系末端与制动组件固接。本发明可以达到使系绳释放装置简化设计及紧凑安装的目的。


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    Titel :

    Tying rope releasing device applied to space tether system


    Weitere Titelangaben:

    一种应用于空间绳系的系绳释放装置


    Beteiligte:
    LIANG FUWEN (Autor:in) / MIAO LONG (Autor:in) / TIAN FENG (Autor:in) / SONG JIAHUI (Autor:in) / BAI SONG (Autor:in) / HE ZIHAO (Autor:in)

    Erscheinungsdatum :

    24.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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