The invention discloses a light-weight open type satellite configuration suitable for batch production. The light-weight open type satellite configuration comprises a main force bearing structure. The optical camera load is mounted in the main bearing structure; the solar wings comprise a fixed solar wing and an unfolded solar wing; the satellite separation support is mounted on the main load-bearing structure; a mounting cabin of the on-satellite single machine is formed between the main force bearing structure and the unfolded solar wing, and a mounting space or a working space of the on-satellite single machine is formed by unfolding or pressing the unfolded solar wing. According to the lightweight open-type satellite configuration suitable for batch production, through satellite-borne integrated design, the envelope size and weight of a satellite are greatly reduced, the open-type mounting surface can greatly improve the structure utilization rate, decoupling between systems is effectively achieved, the final assembly period is effectively shortened, and the lightweight open-type satellite configuration suitable for batch production of satellites is suitable.

    本发明公开了一种适用于批产的轻量化开放式卫星构型,包括主承力结构;安装于所述主承力结构中的光学相机载荷;太阳翼,其包括固定太阳翼和展开太阳翼;安装在所述主承力结构上的卫星分离支座;星上单机,所述主承力结构与所述展开太阳翼之间形成所述星上单机的安装舱,通过所述展开太阳翼的展开或压紧形成对所述星上单机的安装空间或工作空间。本发明的一种适用于批产的轻量化开放式卫星构型通过星载一体化设计,大幅降低了卫星的包络尺寸和重量,敞开式安装面可大幅提升结构利用率,有效实现各系统之间的解耦,有效缩短总装周期,适用于卫星批量生产。


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    Titel :

    Lightweight open type satellite configuration suitable for batch production


    Weitere Titelangaben:

    一种适用于批产的轻量化开放式卫星构型


    Beteiligte:
    CHEN SHANBO (Autor:in) / YANG LIGUO (Autor:in) / ZANG GUOYAN (Autor:in) / XIN JIAN (Autor:in) / GAO FEI (Autor:in) / CHEN MAOSHENG (Autor:in) / ZHANG LEI (Autor:in)

    Erscheinungsdatum :

    24.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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