The present invention relates to a deployment structure separating apparatus for a cube satellite, and more specifically, to a deployment structure separating apparatus for a cube satellite using a pogo pin, which is possible to elastically separate a deployment structure by elasticity of a spring while supplying power capable of cutting a restraint wire by using a pogo pin and is possible to immediately identify a deployment state.

    본 발명은 큐브위성용 전개구조물 분리장치에 관한 것으로, 보다 구체적으로는 포고핀을 이용하여 구속용 와이어를 절단할 수 있는 전원을 공급하는 동시에 스프링의 탄성에 의해 전개구조물을 탄성분리할 수 있고, 전개 상태를 즉시 파악할수 있는 포고핀을 이용한 큐브위성용 전개구조물 분리장치에 관한 것이다.


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    Titel :

    Separation device for deployment sturucture of cubesat using pogo-pin


    Weitere Titelangaben:

    포고핀을 이용한 큐브위성용 전개구조물 분리장치


    Beteiligte:
    OH HYUN UNG (Autor:in) / KIM SU HYEON (Autor:in) / PARK TAE YONG (Autor:in) / SAGONG YOUNG BO (Autor:in) / KIM HONG RAE (Autor:in)

    Erscheinungsdatum :

    11.12.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H02S GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRA-RED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, E.G. USING PHOTOVOLTAIC [PV] MODULES , Erzeugung elektrischer Energie durch Umwandlung von Infrarot-Strahlung, sichtbarem Licht oder ultraviolettem Licht, z.B. unter Verwendung von Photovoltaik [PV]-Modulen




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