The invention provides a flat plate type satellite platform structure which comprises a force bearing frame and a plurality of equipment loads, the force bearing frame is of a hollow structure, and the force bearing frame is integrally formed and is in a flat plate shape; and a plurality of equipment loads are dispersedly carried on the bearing frame. According to the technical scheme, the bearing frame of the flat plate type satellite platform structure has the advantages of being large in size, light in weight, high in rigidity and the like.

    本申请提供一种平板式卫星平台结构,包括承力框架和多个设备载荷,其中,所述承力框架呈镂空结构,且所述承力框架一体成型,呈平板状;多个设备载荷分散搭载于所述承力框架上。本申请的技术方案的平板式卫星平台结构的承力框架具备大尺寸、轻质量和高刚度等特征。


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    Titel :

    Flat plate type satellite platform structure


    Weitere Titelangaben:

    平板式卫星平台结构


    Beteiligte:
    LIU BIN (Autor:in) / YANG WANG (Autor:in) / LONG RUIBO (Autor:in) / CHANG MING (Autor:in) / WANG CHANG'AN (Autor:in) / LIU TONG (Autor:in) / FANG JIE (Autor:in) / DANG YANDONG (Autor:in)

    Erscheinungsdatum :

    15.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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