The invention discloses a flexible satellite platform structure. The flexible satellite platform structure is obtained through transverse and/or longitudinal expansion of a basic configuration. The basic configuration of the flexible satellite platform structure is a polygon prism composed of a connector and rod pieces, wherein the connector is a polyhedron with the top face parallel to the bottomface, a groove is formed in the center of each face of the connector and used for being connected with the rod pieces, the rod pieces comprise the transverse rod pieces and the longitudinal rod pieces, the transverse rod pieces are connected to the side faces of the connector, and the longitudinal rod pieces are connected to the top face and the bottom face of the connector.

    本发明公开一种柔性化卫星平台结构,其通过基本构型进行横向和/或纵向扩展得到。其基本构型为由接头及杆件组成的多棱柱体,其中,接头为底面及底面平行的多面体,其每一面的中心位置均布置有凹槽,用于连接杆件,杆件包括横向杆件及纵向杆件,横向杆件连接于接头的侧面,以及纵向杆件连接于接头的顶面及底面。


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    Title :

    Flexible satellite platform structure


    Additional title:

    一种柔性化卫星平台结构


    Contributors:
    CAO DONGDONG (author) / LIN BAOJUN (author) / AN YANG (author) / CHEN HONGCHENG (author) / TIAN YAN (author) / LIU JIAWEI (author) / XIE FANG (author) / JIANG GUIZHONG (author)

    Publication date :

    2020-12-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS





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