According to the present invention, a satellite body loading apparatus for a thermal vacuum chamber, which is for mounting a satellite body (10) in a thermal vacuum chamber (20), includes: a base frame (110) installed on the ground surface; an upper frame (120) which is horizontally arranged on the upper part of the base frame (110) and has a device rail (121) extended at the upper part and having a rail width corresponding to the chamber rail (21) in the thermal vacuum chamber (20); a lift driving means (130) which is mounted between the base frame (110) and the upper frame (120) and is lifted up and down by using a rotational force of a lifting motor (131) to adjust the arrangement height of the upper frame (120) to arrange the chamber rail (21) and the device rail on the same line; a moving table (140) which is arranged on a front location on the upper frame (120) facing the thermal vacuum chamber (20) to be mounted to and supported by the device rail (121) and move forward and backward while having a mount space unit (141) arranged thereon to mount the satellite body (10) on the upper part; and a driving table (150) which is arranged on a rear location of the moving table (140) on the upper frame, has driving wheels (152) rotated by the rotational force of the driving motor (151) on the lower part to be supported by the device rail (121) and move, thereby pressing the moving table (140) and towing the moving table (140) to move the moving table (140) forward and backward.

    본 발명에 따르면, 열진공챔버(20)의 내부에 위성체(10)를 탑재시키기 위한 열진공챔버용 위성체 로딩장치에 있어서, 지면에 설치되는 베이스프레임(110); 상기 베이스프레임(110)의 상부 위치에 수평배치되며, 상부에는 상기 열진공챔버(20) 내부의 챔버레일(21)과 대응되는 레일폭을 갖는 장치레일(121)이 연장형성된 상부프레임(120); 상기 베이스프레임(110)과 상부프레임(120) 사이에 장착되고, 승강모터(131)의 회전력에 의해 승강구동하면서 상기 챔버레일(21)과 장치레일(121)이 동일선상에 배치되도록 상기 상부프레임(120)의 배치높이를 조절하는 승강작동수단(130); 상기 상부프레임(120) 상에서 열진공챔버(20)와 대향하는 전방 위치에 배치되어 상기 장치레일(121)에 지지되면서 전후방으로 이동가능하게 장착되며, 상부에는 위성체(10)를 탑재하기 위한 안착공간부(141)가 마련된 이동테이블(140); 및 상기 상부프레임(120) 상에서 상기 이동테이블(140)의 후방 위치에 배치되고, 하부에는 구동모터(151)의 회전력에 의해 회전하는 구동바퀴(152)가 장착되어 상기 장치레일(121)에 지지되어 이동하면서 상기 이동테이블(140)을 가압하거나 견인하여 전후방으로 이동시키는 구동테이블(150);을 포함하는 열진공챔버용 위성체 로딩장치를 개시한다.


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    Title :

    SATELLITE LOADING APPARATUS FOR THERMAL VACUUM CHAMBER


    Additional title:

    열진공챔버용 위성체 로딩장치


    Contributors:
    SEO HEE JUN (author) / CHO HYOK JIN (author) / PARK SUNG WOOK (author) / MOON GUEE WON (author)

    Publication date :

    2016-07-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64G Raumfahrt , COSMONAUTICS / B66F HOISTING, LIFTING, HAULING, OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD , Hub-, Verhol- oder Schubvorrichtungen, soweit nicht anderweitig vorgesehen, z.B. Vorrichtungen mit unmittelbarer Krafteinwirkung auf die Last



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