The present invention relates to a micro-satellite having a heat dissipation part, comprising: a frame with an internal space; an electronic equipment part installed in the internal space of the frame; and a heat dissipation part having one side contacting the electronic equipment part in the internal space of the frame and the other side exposed to the outside of the frame, so as to dissipate heat from the electronic equipment part to the outside, wherein the heat dissipation part has different thicknesses for each path for dissipating heat, and can easily dissipate heat from the electronic equipment mounted on the micro-satellite to the outside through the heat dissipation part while reducing the weight of the heat dissipation part.

    본 발명은 내부공간을 가지는 프레임; 상기 프레임의 내부공간에 설치되는 전자장비부; 및 상기 전자장비부의 열을 외부로 방출하도록, 일측이 상기 프레임의 내부공간에서 상기 전자장비부에 접촉하고, 타측이 상기 프레임의 외부로 노출되는 방열부;를 포함하고, 상기 방열부는 열을 방출하기 위한 경로별로 서로 다른 두께를 가지고, 방열부의 무게를 감소시키면서 방열부로 초소형 위성에 탑재된 전자장비부의 열을 외부로 용이하게 방출시킬 수 있다.


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    Title :

    NANO SATELLITE HAVING RADIATING DEVICE


    Additional title:

    방열부를 구비하는 초소형 위성


    Contributors:
    RYU JUN SUK (author)

    Publication date :

    2023-07-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

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



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