The invention provides a satellite fixing structure based on a one-rocket-double-satellite parallel launching mode and a mounting system thereof, which are used for a satellite in the one-rocket-double-satellite parallel launching mode, and are used for promoting the realization of the satellite fixing structure by using a set of simple and convenient solar wing design structure, so that the required production cost is remarkably reduced.

    本申请提供了一种基于一箭双星并联发射方式的卫星固定结构及其安装系统,用于为一箭双星并联发射方式的卫星,以一套精简且简便的太阳翼设计结构促进卫星固定结构的实现,从而显著降低所需的生产成本。


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    Titel :

    Satellite fixing structure based on one-rocket double-satellite parallel launching mode and mounting system thereof


    Weitere Titelangaben:

    基于一箭双星并联发射方式的卫星固定结构及其安装系统


    Beteiligte:
    XU HANG (Autor:in) / DUAN XIAO (Autor:in) / WANG HAOQING (Autor:in) / WANG ZICHENG (Autor:in) / YAN HAIPING (Autor:in)

    Erscheinungsdatum :

    2022-10-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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