The invention provides a support of a star sensor and belongs to the technical field of aerospace equipment. With the support adopted, the problem that an existing star sensor is poor in heat dissipation performance and large in temperature control difficulty is solved. The support of the star sensor comprises a support body used for supporting the star sensor; the support body is made of a heat conduction material and provided with a device cavity; and a phase change energy storage medium used for temperature control is arranged in the device cavity. With the support of the star sensor adopted, the heat dissipation performance of the star sensor is good.

    本发明提供了一种星敏感器的支架,属于航天设备技术领域。它解决了现有星敏感器散热性能差、控温难度大的问题。本星敏感器的支架包括用于支撑星敏感器的架体,架体由导热材料制成且具有装置腔,装置腔内设有用于控温的相变蓄能介质。本星敏感器的支架具有使星敏感器散热好的优点。


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    Titel :

    Support of star sensor


    Weitere Titelangaben:

    一种星敏感器的支架


    Beteiligte:
    ZHANG JINGJING (Autor:in) / LIU WU (Autor:in) / CHEN LONG (Autor:in) / QIN GUIJUN (Autor:in) / WANG DONGSHEN (Autor:in) / YANG DAOJUN (Autor:in)

    Erscheinungsdatum :

    2020-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H05K PRINTED CIRCUITS , Gedruckte Schaltungen



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