A separation device for a launcher according to an embodiment of the present invention comprises: an one side upper portion housing; a separation pin provided with a holding protrusion; a rotation key including a rotation portion and an extension portion downwardly extended from a lower end of the rotation portion; a lower portion housing coupled to a lower portion of the one side upper portion housing; a fixing key located in a third guide space of the one side upper portion housing at an upper end part thereof; an elastic member located in a guide groove; and a rotation limiting member located between the extension portion and the fixing key, thereby capable of reducing and simplifying a driving distance of the separation device by using the elastic member.

    본 발명의 실시예에 따른 발사체용 분리장치는, 일측 상부 하우징; 걸림돌기가 구비되는 분리핀; 회전부 및 상기 회전부의 하단으로부터 하향 연장되는 연장부를 포함하는 회전키; 상기 일측 상부 하우징의 하부에 결합되는 하부 하우징; 상단 부위가 상기 일측 상부 하우징의 제3 가이드 공간에 위치하는 고정키; 상기 가이드 홈에 위치되는 신축부재; 및 상기 연장부와 상기 고정키 사이에 위치하는 회전제한부재; 를 포함한다.


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    Title :

    SEPARATION DEVICE FOR LAUNCHER


    Additional title:

    발사체용 분리장치


    Contributors:

    Publication date :

    2018-02-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen / B64G Raumfahrt , COSMONAUTICS



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