The invention provides a load structure integrated open type satellite configuration which comprises a platform structure and a load structure, the platform structure comprises a bottom plate, a first side plate, a second side plate, a first stringer and a second stringer, and the load structure comprises a first load and a second load. The bottom plate, the first side plate, the second side plate, the first load, the second load, the first stringer and the second stringer define an open type isosceles trapezoid main body structure. The satellite constellation test platform has the beneficial effects that the open isosceles trapezoid main body structure is adopted, the general assembly operation space is large, the test flexibility is high, the requirements of satellite constellation automatic assembly production and batch test can be effectively met, a load structure and a platform structure are integrated, and the structural weight is reduced.

    本发明提供了一种载荷结构一体化开敞式卫星构型,包括平台结构和载荷结构,所述平台结构包括底板、第一侧板、第二侧板、第一桁条和第二桁条,所述载荷结构包括第一载荷和第二载荷,所述底板、第一侧板、第二侧板、第一载荷、第二载荷、第一桁条和第二桁条围合形成开敞式等腰梯形主体结构。本发明的有益效果是:采用开敞式等腰梯形主体结构,总装操作空间大、测试灵活性高,可有效满足卫星星座自动化装配生产和批量化测试的要求,将载荷结构与平台结构一体化,降低了结构重量。


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    Titel :

    Load structure integrated open type satellite configuration


    Weitere Titelangaben:

    一种载荷结构一体化开敞式卫星构型


    Beteiligte:
    LIU XUEFENG (Autor:in) / GAO GE (Autor:in) / HAN FEI (Autor:in) / TANG XINCHUN (Autor:in) / WEI SHILONG (Autor:in) / GUO BIBO (Autor:in)

    Erscheinungsdatum :

    2023-01-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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