PROBLEM TO BE SOLVED: To provide a space environment testing device capable of testing a test object in a simulated space environment in which a temperature is set at 10K or lower.SOLUTION: A space environment testing device includes: a second cylindrical shroud 42 which is housed in a first shroud 31, both the ends of which are formed as closed ends, and which is extended in an X-direction; a test object loading table 45 which is arranged within the second shroud 42 and which is loaded with a test object 14; and a refrigeration machine 56 which is arranged on the inside with respect to the first shroud 31 and which includes a cold head 56-3 for cooling the test object 14 via the second shroud 42.

    【課題】本発明は、温度が10K以下とされた模擬宇宙空間において、被試験体の試験を行うことの可能な宇宙環境試験装置を提供することを課題とする。【解決手段】第1のシュラウド31内に収容され、両端が閉塞端とされ、X方向に延在する筒状の第2のシュラウド42と、第2のシュラウド42内に配置され、被試験体14が載置される被試験体載置台45と、第1のシュラウド31よりも内側に配置され、第2のシュラウド42を介して、被試験体14を冷却するコールドヘッド56−3を含む冷凍機56と、を有する。【選択図】図1


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    Titel :

    SPACE ENVIRONMENT TESTING DEVICE


    Weitere Titelangaben:

    宇宙環境試験装置


    Beteiligte:
    MIYAI REI (Autor:in)

    Erscheinungsdatum :

    22.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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