The invention provides an integrated satellite compact in layout. The integrated satellite comprises a bottom plate, and a mounting flange is arranged on the surface of the bottom plate; the mounting flange is used for arranging of an inner-satellite load device, and therefore a first force transmission path for the inner-satellite load device is formed. The four opposite angles of the surface of the bottom plate are each provided with a partition plate, and a top plate is supported by the four partition plates; and an outer-satellite load device is arranged on the top plate, and therefore a second force transmission path for the outer-satellite load device is formed. The integration satellite compact in layout has the beneficial effects that the integrated satellite configuration with the load as the center is provided, and the scheme of carrying out layout around the load is achieved; and meanwhile, the structural scheme with two main force transmission paths and one secondary force transmission path for the combined action is designed, the mechanic environment of the loads is optimized, the design complexity and the design pressure of a satellite structure and a load structure are reduced, and the bearing ratio of the satellite structure is improved.


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    Titel :

    Integration satellite compact in layout


    Beteiligte:
    ZHANG WENQIAO (Autor:in) / SONG WEIXU (Autor:in) / ZHU ZHENCAI (Autor:in) / LI HUAWANG (Autor:in) / ZHU CHENG (Autor:in) / WANG JIANPING (Autor:in)

    Erscheinungsdatum :

    13.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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