Spacecraft generally operates in vacuum and deep cold environment. Some special planetary surface detectors, such as Mars surface detectors may operate in atmospheric environment. Spacecraft receives orbital heat flux in such forms as solar radiation, planetary (lunar) albedo radiation and planetary (lunar) infrared radiation and dissipate heat through the spacecraft heat rejection surface to the deep cold space. This process finally leads to the dynamic balance of temperature.


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    Title :

    Spacecraft Thermal Testing


    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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