The invention provides a stationary orbit ultra-large type assemblable satellite platform configuration, which belongs to the technical field of spacecrafts, and comprises a mother platform, a transition sub-platform I and a transition sub-platform II, a functional sub-platform I and a functional sub-platform II, a functional sub-platform III and a functional sub-platform IV, an energy module I and an energy module II, and a mechanical arm I and a mechanical arm II, wherein the mother platform is a control center of a whole satellite; the transition sub-platform I and the transition sub-platform II are respectively connected with the mother platform through connecting devices; the functional sub-platform I and the functional sub-platform II are respectively connected with the transition sub-platform I through connecting devices; the functional sub-platform III and the functional sub-platform IV are respectively connected with the transition sub-platform II through connecting devices; the energy module I and the energy module II are respectively connected with the transition sub-platform I and the transition sub-platform II through connecting devices to supply power; the mechanicalarm I and the mechanical arm II are installed on the transition sub-platform I and the transition sub-platform II correspondingly to execute an on-orbit assembling task. The platform configuration issuitable for expansion, can adapt to on-orbit construction of large satellites with the on-orbit flight weight of 10-20 t, is applied to various types of satellites and service stations, and is wide in application range.

    本发明提供了一种静止轨道超大型可组装卫星平台构型,属于航天器技术领域,包括母平台,为整星的控制中心;过渡子平台Ⅰ、过渡子平台Ⅱ分别与母平台通过连接装置连接;功能子平台Ⅰ、功能子平台Ⅱ分别与过渡子平台Ⅰ通过连接装置连接;功能子平台Ⅲ、功能子平台Ⅳ分别与过渡子平台Ⅱ通过连接装置连接;能源模块Ⅰ、能源模块Ⅱ分别与过渡子平台Ⅰ、过渡子平台Ⅱ通过连接装置连接,提供电源;机械臂Ⅰ、机械臂Ⅱ分别安装于过渡子平台Ⅰ、过渡子平台Ⅱ上,执行在轨组装任务。本发明平台构型适合扩展,能够适应在轨10‑20t飞行重量的大型卫星在轨构建,应用于多种类型的卫星和服务站,应用范围广泛。


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    Titel :

    Stationary orbit ultra-large type assemblable satellite platform configuration and on-orbit assembly method


    Weitere Titelangaben:

    静止轨道超大型可组装卫星平台构型以及在轨组装方法


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

    Erscheinungsdatum :

    2020-07-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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