The invention discloses a configuration method of an efficient and compact serial satellite platform, the serial satellite platform comprises a main bearing structure 1, a load instrument cabin 2, a platform instrument cabin 3, a solar wing 4, a thruster 5 and a measurement and control antenna 6, when the serial satellite platform is installed on a carrier rocket to be launched, the serial satellite platform is in a folded state, and when the serial satellite platform is installed on the carrier rocket to be launched, the serial satellite platform is in a non-folded state; and the serial satellite platform is converted into an unfolded state after the carrier rocket and the main satellite are transferred to a specified orbit position in the space. In the invention, aiming at the market demand of low-cost carrying and launching in China, the configuration layout method of the serial carrying and launching satellite platform matched with the current carrier rocket interface requirement, the large satellite platform interface requirement and the apogee orbital transfer working mode in China is designed; the configuration method of the satellite platform for serial carrying launching, which adapts to the requirements of current carrier rocket interfaces in China, adapts to the requirements of large communication satellite interfaces in China and is matched with an apogee orbital transfer working mode, is realized.

    本发明公开了一种高效紧凑的串行式卫星平台的构形方法,串行式卫星平台包括主承力结构1、载荷仪器舱2、平台仪器舱3、太阳翼4、推力器5和测控天线6,所述串行式卫星平台安装在运载火箭上准备发射时,处于收拢状态,所述串行式卫星平台在运载火箭和主星转移至在太空中指定轨道位置后,转换为展开状态。本发明中,针对我国低成本搭载发射的市场需求,设计出一种与我国当前运载火箭接口要求、大型卫星平台接口要求及远地点变轨工作模式相匹配的串行式搭载发射卫星平台的构型布局方法,实现了一种适应我国当前运载火箭接口要求、适应我国大型通信卫星接口要求及远地点变轨工作模式相匹配的用于串行式搭载发射的卫星平台的构型方法。


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    Title :

    Configuration method of efficient and compact serial satellite platform


    Additional title:

    一种高效紧凑的串行式卫星平台的构形方法


    Contributors:
    ZOU SHUANG (author) / LIU HUILIANG (author) / LYU HONGJIAN (author) / SUN QIAN (author) / PI XIAOLI (author) / LI ZHENGJU (author) / LI QIANG (author) / WANG RAN (author) / LIU AIDONG (author)

    Publication date :

    2023-09-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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