The present invention relates to rocket technology, and more specifically, to a rocket fixing detent structure applied to a rocket mounted on an air launched platform to be launched and a rocket having the same. The fixing detent structure of the present invention includes a substrate, a detent device, a compressive force adding device, and a posture control support device.

    본 발명은 로켓 기술에 관한 것으로서, 더 상세하게는 공중발사 플랫폼에 탑재되어 발사되는 로켓에 적용되는 로켓 고정용 디텐트 구조 및 이를 갖는 로켓에 대한 것이다.


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    Titel :

    Fixing detent structure and Rocket having the same


    Weitere Titelangaben:

    고정용 디텐트 구조 및 이를 갖는 로켓


    Beteiligte:
    CHOI HOON SEOK (Autor:in) / KIM KI HONG (Autor:in)

    Erscheinungsdatum :

    2019-07-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F41F APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS , Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze



    Rocket Detent and Release Mechanism

    B. H. Campbell / E. J. DeBona / W. J. Laird | NTIS | 1978


    Rocket Detent and Release Mechanism

    B. H. Campbell / E. J. Debona / W. J. Laird | NTIS | 1978


    DUAL DETENT APPARATUS FOR ROCKET

    LEE JUN HO / BAE MIN JI / KIM YOUNG IL et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Automatic Hard-Soft Rocket Detent System

    J. M. Madderra | NTIS | 1981


    PIN DETENT STRUCTURE

    SAKAI KEIJI / ICHIKAWA YASUO / OBATA TETSUYA et al. | Europäisches Patentamt | 2021

    Freier Zugriff