The invention provides a satellite assembling method. The method comprises the following satellite assembling processes after finishing satellite prototype sample design, structural drawing making, satellite commissioning, satellite production and satellite acceptance work, and comprises the following steps of carrying out integration test assembly, forming an integration test whole satellite, and carrying out tests in multiple states; carrying out thermal test modification on the basis of the integration test whole satellite to form a thermal test whole satellite; performing environmental test modification on the basis of the thermal test whole satellite to form an environmental test whole satellite; on the basis of the environmental test whole satellite, carrying out test modification before delivery and delivery modification to form a final whole satellite to be launched.

    本发明提供了一种卫星装配方法,包括:完成卫星初样设计、结构图纸的绘制、卫星投产、卫星生产和卫星验收工作后,进行以下卫星装配流程,包括:进行集成测试装配,形成集成测试整星,进行多个状态下的测试;在集成测试整星的基础上,进行热试验改装,形成热试验整星;在热试验整星的基础上,进行环境试验改装,形成环境试验整星;在环境试验整星的基础上,进行出厂前测试改装和出厂改装,形成最终的待发射整星。


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    Title :

    Satellite assembling method


    Additional title:

    卫星装配方法


    Contributors:
    CAO DONGDONG (author) / AN YANG (author) / CHEN HONGCHENG (author) / LIN BAOJUN (author) / TIAN YAN (author) / LIU JIAWEI (author) / XIE FANG (author) / SHEN YUAN (author) / JIANG GUIZHONG (author)

    Publication date :

    2021-04-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / B64G Raumfahrt , COSMONAUTICS



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