The optical remote sensing satellite comprises a satellite box body, a satellite sailboard and a remote sensing camera, a left side plate and a right side plate of the satellite box body are each of a first right trapezoid structure, and the lower end of a front plate and the lower end of a rear plate are perpendicularly fixed to the front side edge and the rear side edge of a bottom plate respectively; the right-angle waists of the left side plate and the right side plate are vertically fixed to the left side and the right side of the bottom plate, the left side and the right side of the front plate are fixedly connected with the left side plate and the right side plate respectively, and the left side and the right side of the rear plate are fixedly connected with the left side plate and the right side plate respectively. The front side edge of the top plate is fixed to the top end of the front plate, the top plate is parallel to the bottom plate, the rear side edge of the top plate is fixedly connected with the rear plate, and the left side edge and the right side edge of the top plate are fixedly connected with the left side plate and the right side plate respectively. A horizontally-arranged reinforcing plate is further fixed to the front side face of the rear plate. The remote sensing camera is fixed on the outer surface of the top plate; satellite sailboards are respectively hinged to the outer surfaces of the left side plate and the right side plate; and a plurality of hanging structures are arranged on the rear side surface of the rear plate.

    本发明涉及一种侧挂式构型的光学遥感卫星,包括卫星箱体、卫星帆板和遥感相机,卫星箱体的左侧板和右侧板均呈第一直角梯形结构,前板和后板的下端分别垂直固定在底板的前侧边和后侧边,左侧板和右侧板的直角腰垂直固定在底板的左侧边和右侧边,前板的左右两侧边分别与左侧板和右侧板固定连接,后板的左右两侧边分别与左侧板和右侧板固定连接;顶板的前侧边固定在前板的顶端,顶板与底板平行布置,顶板的后侧边与后板固定连接,顶板的左侧边和右侧边分别与左侧板和右侧板固定连接;后板的前侧面还固定有水平布置的加强板;遥感相机固定在顶板的外表面上,左侧板和右侧板的外表面上分别铰接有卫星帆板;后板的后侧面设有多个挂接结构。


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    Titel :

    Optical remote sensing satellite with side hanging type configuration


    Weitere Titelangaben:

    一种侧挂式构型的光学遥感卫星


    Beteiligte:
    KONG LINGBO (Autor:in) / GAO ENYU (Autor:in) / HU BAOYI (Autor:in) / YAN ZHOU (Autor:in)

    Erscheinungsdatum :

    07.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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