The invention provides a spacecraft thermal control structure and a spacecraft, provides a thermal control scheme which is compact in structure and can be directly installed, and can better meet the working temperature requirements of thermal insulation, refrigeration, heating and temperature equalization of a temperature-sensitive single machine.

    本申请提供了一种航天器热控结构以及航天器,提供了一种结构紧凑、可直接安装的热控方案,且可以较好地满足温度敏感单机其隔热、制冷、加热和均温的工作温度需求。


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    Title :

    Spacecraft thermal control structure and spacecraft


    Additional title:

    一种航天器热控结构以及航天器


    Contributors:
    WANG ZICHENG (author) / DUAN XIAO (author) / WANG HAOQING (author) / XU HANG (author) / YAN HAIPING (author)

    Publication date :

    2022-10-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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