The purpose of spacecraft thermal control is, according to the requirements of a flight mission and the condition of internal and external thermal loads to which the spacecraft is exposed in the whole life cycle, to systematically take thermal control measures to organize the heat exchange processes inside and outside the spacecraft so as to keep the temperature of onboard equipments, structures and living environment within the prescribed limits.


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    Title :

    Design of Spacecraft Thermal Control Subsystem


    Additional title:

    sp.


    Contributors:
    Miao, Jianyin (author) / Zhong, Qi (author) / Zhao, Qiwei (author) / Zhao, Xin (author)


    Publication date :

    2020-08-20


    Size :

    20 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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