A heat control structure includes a heat insulator disposed between a housing for accommodating a heat control target mounted on a satellite and the heat control target. The heat insulator is disposed so as to be in contact with the housing and the heat control target, the heat insulator contains at least silica aerogel, and the heat insulator has a thermal resistance of 0.02 (m2·K)/W or more.


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    Title :

    HEAT CONTROL STRUCTURE AND SATELLITE HAVING THE SAME


    Contributors:
    CHO MENGU (author) / MASUI HIROKAZU (author) / OIKAWA KAZUMA (author) / KUWABARA RYOU (author) / TSURUTA TAKASHI (author) / MORI MASATO (author)

    Publication date :

    2025-04-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16L PIPES , Rohre / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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