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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    Titel :

    Design of Spacecraft Thermal Control Subsystem


    Weitere Titelangaben:

    sp.


    Beteiligte:
    Miao, Jianyin (Autor:in) / Zhong, Qi (Autor:in) / Zhao, Qiwei (Autor:in) / Zhao, Xin (Autor:in)


    Erscheinungsdatum :

    20.08.2020


    Format / Umfang :

    20 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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