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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    Titel :

    Spacecraft Thermal Testing


    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




    Spacecraft thermal vacuum testing

    Elam, B. F. / Lancaster, L. D. | NTRS | 1972


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    Ercol, C. J. / Krein, S. J. | British Library Conference Proceedings | 1997


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    ZAJTSEV SERGEJ EDUARDOVICH / POZHALOV VYACHESLAV MIKHAJLOVICH / SMIRNOV ALEKSANDR SERGEEVICH et al. | Europäisches Patentamt | 2020

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