The invention provides a stationary orbit ultra-large type assembling satellite platform configuration. The configuration comprises a mother platform, a first module cabin, a second module cabin, a first functional cabin, a second functional cabin, a first connecting truss, a second connecting truss, a first energy module, a second energy module, a first mechanical arm and a second mechanical arm,wherein the mother platform carries out comprehensive management and control on a whole satellite; the first module cabin and the second module cabin are connected with the mother platform and are used for providing a mounting platform for a ultra-large platform single-machine module; the first functional cabin and the second functional cabin are connected with the first module cabin and the second module cabin and are used for carrying a working load; the first connecting truss and the second connecting truss are mounted on the first energy module and the second energy module respectively; and the first mechanical arm and the second mechanical arm are installed on an east side and a west side of the mother platform correspondingly. The configuration can be used for an ultra-large comprehensive satellite platform, on-orbit maintenance of the satellite platform is facilitated, development cost is low, a platform configuration space is open, and energy utilization efficiency is high.

    本发明提供了一种静止轨道超大型可组装卫星平台构型,包括:母平台,母平台对整个卫星进行综合管控;第一模块舱和第二模块舱,第一模块舱和第二模块舱与所述母平台相连接,为超大型平台单机模块提供安装平台;第一功能舱和第二功能舱,第一功能舱和第二功能舱分别与第一模块舱和第二模块舱连接,用来搭载工作载荷;第一连接桁架和第二连接桁架、第一能源模块和第二能源模块,第一连接桁架和第二连接桁架分别安装在所述第一能源模块和第二能源模块上;第一机械臂和第二机械臂,第一机械臂和第二机械臂分别安装在母平台的东面和西面。本发明可用于超大型综合卫星平台,便于卫星平台进行在轨维护,研制成本低,平台构型空间开放,能源利用效率高。


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    Titel :

    Stationary orbit ultra-large type assembling satellite platform configuration and assembling method


    Weitere Titelangaben:

    一种静止轨道超大型可组装卫星平台构型及装配方法


    Beteiligte:
    YANG LILI (Autor:in) / LI WENLONG (Autor:in) / KONG XIANGLONG (Autor:in) / XU HAO (Autor:in) / QIAN YONG (Autor:in)

    Erscheinungsdatum :

    25.08.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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