The present invention relates to a projectile, comprising: a housing in which a satellite is accommodated, and which includes an outlet for ejecting the satellite; a door which is connected to the housing to be rotatable, and selectively opens and closes the outlet; a guide part which is disposed inside the housing and guides the motion of the satellite when the satellite is ejected; a link part which is connected to the housing and connected to the guide part; a linear motion part which is connected to the link part and moves in a linear motion; and a restraining part which is connected to the door and selectively restrains the linear motion part.

    본 발명은 위성이 수납되며, 상기 위성이 사출되는 출구를 포함한 하우징과, 상기 하우징에 회동 가능하게 연결되며, 상기 출구를 선택적으로 개폐하는 도어와, 상기 하우징 내부에 배치되며, 상기 위성의 사출 시 상기 위성의 운동을 가이드하는 가이드부와, 상기 하우징에 회동 가능하게 연결되며, 상기 가이드부와 연결되는 링크부와, 상기 링크부와 연결되며, 선형 운동하는 선형운동부와, 상기 도어에 연결되어 상기 선형운동부를 선택적으로 구속하는 구속부를 포함하는 발사체를 개시한다.


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    Title :

    Satellite launch vehicle


    Additional title:

    위성용 발사체


    Contributors:
    KIM MIN KI (author) / KIM HAE DONG (author) / CHOI WON SUB (author) / CHO DONG HYUN (author) / KIM JIN HYUNG (author)

    Publication date :

    2021-07-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / E05B LOCKS , Schlösser



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