The invention relates to a satellite cooling system and a satellite. The satellite cooling system comprises a cold plate used for bearing the load of a satellite, and the cold plate is provided with a cooling flow channel; the circulating pump is arranged on the cold plate and communicates with the cooling flow channel; and the fluid controller is arranged on the cold plate, and the fluid controller is electrically connected with the circulating pump so as to control the circulating pump. The cold plate is used for supporting all loads of the satellite, the cooling flow channel in the cold plate serves as a channel of the liquid working medium, the liquid working medium can absorb heat of the loads, the temperature of all the loads of the satellite is made to be uniform, and the temperature uniformity of the satellite is improved.

    本申请涉及一种卫星冷却系统及卫星。卫星冷却系统包括:冷板,用于承载卫星的载荷,冷板设置有冷却流道;循环泵,设置于冷板,循环泵连通冷却流道;流体控制器,设置于冷板,流体控制器与循环泵电连接,以控制循环泵。本申请的冷板设置用于支撑卫星的各个载荷,冷板上的冷却流道作为液体工质的通道,液体工质能够吸收载荷的热量,使得卫星各个载荷的温度较为均匀,提高卫星的均温性。


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    Titel :

    Satellite cooling system and satellite


    Weitere Titelangaben:

    一种卫星冷却系统及卫星


    Beteiligte:
    YANG PENG (Autor:in) / QIU SHAOJIE (Autor:in) / DING TING (Autor:in) / ZHI JIAYUN (Autor:in) / XU CHENG (Autor:in) / MA CHAOYANG (Autor:in) / ZHENG TONG (Autor:in) / ZHOU ZIYANG (Autor:in) / YANG QIAOLONG (Autor:in) / CHANG MING (Autor:in)

    Erscheinungsdatum :

    2024-01-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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