The present invention provides a constant temperature maintaining device for a space environment test, which comprises: a heat vacuum chamber vacuum-processed therein; a constant temperature module part arranged adjacent to a part of test components so as to heat or cool the part of the test components; and a power supply part supplying power to the constant temperature module part, wherein the constant temperature module part includes a thermoelement allowing heat to be moved from one surface to the other surface when electric currents flow by the power supply part. The constant temperature module part forms a temperature deviation in the test components by heating or the cooling the part of the test components when the power is supplied from the power supply part. Therefore, the constant temperature maintaining device for a space environment test is configured to copy a space environment.

    본 발명은 내부가 진공 처리되는 열진공챔버와, 시험 부품의 일부 영역을 가열하거나 냉각하기 위해 상기 시험 부품의 상기 일부 영역에 근접하게 배치되는 항온모듈부와, 및 상기 항온모듈부에 전원을 공급하는 전원 공급부를 구비하고, 상기 항온모듈부는, 상기 전원 공급부에 의해 전류가 흐르면 일 면에서 다른 면으로 열이 이동하는 열전소자를 포함하고, 상기 항온모듈부는 상기 전원 공급부로부터 전원이 공급되면, 상기 시험 부품의 상기 일부 영역을 가열 또는 냉각시켜 상기 시험 부품에게 온도 편차를 형성해줌으로써 우주 환경을 모사하도록 이루어진 우주 환경 시험용 항온 유지 장치를 제공한다.


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    Titel :

    Temperature maintaining device for space environmental test


    Weitere Titelangaben:

    우주 환경 시험용 항온 유지 장치


    Beteiligte:
    KIM KYUNG KEUN (Autor:in) / SEO HEEJUN (Autor:in) / CHO HYOKJIN (Autor:in) / PARK SUNG WOOK (Autor:in) / YI HYE JIN (Autor:in)

    Erscheinungsdatum :

    2020-07-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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



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