The invention provides a cabin section structure type satellite which comprises a platform cabin, a load cabin, a top plate, a plurality of devices, a solar wing and a star sensor head support, the platform cabin and the load cabin are both of a frame type structure, the middle of the platform cabin and the middle of the load cabin are both cavities, the load cabin is installed at the top of the platform cabin, and the top plate is installed at the top of the load cabin. The multiple devices are installed on the inner side wall of the platform cabin and the inner side wall of the load cabin, and the solar wing and the star sensor head support are both installed on the outer side wall of the platform cabin. No partition plate is arranged in the middle, space is fully utilized, equipment is installed on the side plates, installation of the equipment on the side plates can be independently and parallelly carried out, rapid assembly is achieved, and rapid equipment replacement can be achieved by opening the side plates. The structure is simple, assembling is convenient, and batch machining can be achieved. The spacecraft with one or more functions can be rapidly manufactured and launched in an integrated mode, and only different load cabins are needed for different tasks. The whole process of task setting, assembly testing, transportation launching and on-orbit service can be rapidly completed.

    本发明提供了一种舱段结构式卫星,包括:平台舱、载荷舱、顶板、多个设备、太阳翼、星敏头部支架、平台舱以及载荷舱均为框架式结构,平台舱以及载荷舱的中部均为空腔,载荷舱安装在平台舱的顶部,顶板安装在载荷舱的顶部,多个设备安装在平台舱的内侧壁以及载荷舱的内侧壁上,太阳翼以及星敏头部支架均安装在平台舱的外侧壁上。中间没有隔板,空间得到充分利用,在侧板上安装设备,各侧板上设备的安装可以独立并行进行,实现快速组装,可打开侧板实现快速设备更换。结构简单、装配方便,可批量加工。能够快速集成制造、发射一种或者多种功能的航天器,不同任务仅需不同的载荷舱。可快速完成任务设置、组装测试、运输发射、在轨服务全流程。


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    Titel :

    Cabin section structure type satellite


    Weitere Titelangaben:

    一种舱段结构式卫星


    Beteiligte:
    DONG SUHUI (Autor:in) / SUN GUOFEI (Autor:in) / HE CHANG'AN (Autor:in) / SONG KEJIAN (Autor:in) / CHEN SHUHUI (Autor:in) / YANG HONGMING (Autor:in) / WANG LIPING (Autor:in) / KANG WEIWEI (Autor:in) / QI JING (Autor:in) / ZHANG YAOYAO (Autor:in)

    Erscheinungsdatum :

    2023-08-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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