The invention provides a satellite on-orbit automatic shading thermal control device and a satellite thereof, and belongs to the technical field of spacecraft thermal control. The satellite on-orbit automatic shading thermal control device comprises a satellite body mechanism, an automatic unfolding and folding mechanism and a wave-transparent heat dissipation baffle. The star body mechanism is connected with the wave-transparent heat dissipation baffle through the automatic unfolding and folding mechanism, the wave-transparent heat dissipation baffle comprises wave-transparent nanometer thermal control films and a wave-transparent honeycomb, and the wave-transparent nanometer thermal control films are arranged on the two planes of the wave-transparent honeycomb. Reflection of a satellite to the floor is greatly reduced, light is effectively shielded, the heat dissipation area is increased, and satellite sun shading and heat dissipation are facilitated.

    本发明提供了航天器热控制技术领域一种卫星在轨自动遮光热控装置及其卫星,包括星体机构、自动展收机构以及透波散热挡板;所述星体机构通过所述自动展收机构与所述透波散热挡板连接设置,所述透波散热挡板包括透波纳米热控薄膜和透波蜂窝,所述透波纳米热控薄膜设置在所述透波蜂窝两平面设置。本发明大幅减少卫星对地板的反光,有效遮光并增加散热面积,有利于卫星遮阳和散热。


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    Titel :

    Satellite on-orbit automatic shading thermal control device and satellite thereof


    Weitere Titelangaben:

    卫星在轨自动遮光热控装置及其卫星


    Beteiligte:
    CHEN ZHANSHENG (Autor:in) / FU XIN (Autor:in) / ZHAI ZAITENG (Autor:in) / CHEN HAN (Autor:in) / LAI JING (Autor:in) / ZHOU BILEI (Autor:in) / YANG MINGBO (Autor:in) / ZHAO YANBIN (Autor:in) / SUN JIE (Autor:in) / ZOU XING (Autor:in)

    Erscheinungsdatum :

    01.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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