A projectile landing device for recovering a projectile according to an embodiment includes a plurality of grippers spaced apart from each other, wherein the gripper comprises: a support; a guide having one side connected to one end of the support; and a shock absorber having one end connected to the other end of the support, and the other end connected to the other end of the guide. The projectile can be guided and the load is buffered so that the projectile can be safely recovered.

    일 실시예에 따른 발사체를 회수하는 발사체 착륙 장치는, 이격되어 배치되는 복수 개의 그리퍼를 포함하고, 상기 그리퍼는, 지지대; 상기 지지대의 일 단에 일 측이 연결되는 가이드; 및 상기 지지대의 타 단에 일 단이 연결되고, 상기 가이드의 타 측과 타 단이 연결되는 완충기를 포함하며, 상기 발사체를 안내하고 하중을 완충시켜 안전하게 회수할 수 있다.


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    Titel :

    PROJECTILE LANDING APPARATUS TO RETRIEVE PROJECTILE


    Weitere Titelangaben:

    발사체를 회수하는 발사체 착륙 장치


    Beteiligte:
    IM SUNG HYUCK (Autor:in) / LEE JUN SEONG (Autor:in) / LEE KEE JOO (Autor:in) / PARK JAE SUNG (Autor:in)

    Erscheinungsdatum :

    20.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16F SPRINGS , Federn



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