The present invention includes: a first body part supported on a projectile; an ejection part installed in the first body to eject a microsatellite; a second body part spaced apart from the first body part and supported by the projectile; and a connection part connecting the first body part and the second body part, thereby capable of stably supporting the microsatellite and then launching the microsatellite. The present invention provides a microsatellite launch apparatus that can be made lightweight by reducing the weight thereof.

    본 발명은 발사체에 지지되는 제1 몸체부; 초소형 위성을 사출할 수 있도록, 상기 제1 몸체부에 설치되는 사출부; 상기 제1 몸체부와 이격되고, 상기 발사체에 지지되는 제2 몸체부; 및 상기 제1 몸체부와 상기 제2 몸체부 사이를 연결하는 연결부;를 포함하고, 초소형 위성을 안정적으로 지지하다가 사출시킬 수 있다.


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    Title :

    NANO SATELLITE LAUNCH APPARATUS


    Additional title:

    초소형 위성 사출장치


    Contributors:

    Publication date :

    2023-07-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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