A missile nut assembled side jet thruster according to the present invention includes a nut position hole (1-2) bored on a missile body (1), a nozzle which is formed on a propellant filler (3) to provide the side jet thrust of a missile and has a male screw (3-1A), and a fixing nut (10) which is fixed to the nozzle (3-1) by screwing a female screw (10-1) formed on an inner circumference thereof with a male screw (3-1A). Thereby, the present invention maintains the advantage of an I-type pulse side jet thruster, prevents the degradation of inner space efficiency and the increase of a weight due to the thickness of the missile body (1) and, particularly, solves the difficulty of constantly maintaining an igniter wire direction by assembling the side jet thruster through rotation.

    본 발명의 유도탄 너트 조립형 측 추력기에는 유도탄 동체(1)에 뚫린 너트 위치홀(1-2), 유도탄의 측 추력을 제공하는 추진제 충전체(3)에 구비되어 수나사(3-1A)를 형성한 노즐(3-1), 내주면으로 형성된 암나사(10-1)가 수나사(3-1A)와 나사 체결되어 노즐(3-1)과 고정되는 고정 너트(10)가 포함됨으로써 'I' 타입의 펄스형 측 추력기 장점을 유지하면서도 유도탄 동체(1)의 두께로 인한 무게 증가와 내부 공간 효율성 저하를 방지하고, 특히 측추력기의 회전조립에 의한 점화기 배선 방향의 일정한 유지 어려움도 해소되는 특징을 갖는다.


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    Title :

    MISSILE NUT ASSEMBLING TYPE SIDE THRUST VECTOR DEVICE


    Additional title:

    유도탄 너트 조립형 측 추력기


    Contributors:
    LEE DONG JU (author) / KIM JAI HA (author) / SON YOUNG IL (author) / HONG SEOK HYUN (author) / CHOI SEUNG HYUK (author)

    Publication date :

    2015-11-16


    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 / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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    Sahinkaya, Y. E. / Cordova, S. A. / International Federation of Automatic Control | British Library Conference Proceedings | 1995



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