According to one embodiment of the present invention, provided is a small launch vehicle equipped with a recoverable mission payload including a mission payload, a fuselage on which the mission payload is loaded, and a nose cone covering an upper part of the fuselage. The small launch vehicle equipped with a recoverable mission payload comprises: a recovery device mounted on the mission payload; and a support plate which supports the mission payload and can slide in the vertical direction of the fuselage. The recovery device includes: a rotation shaft connected to the mission payload and rotatable relative to the mission payload; and a plurality of rotors radially connected to a rotation axis.

    본 발명의 한 실시예에 따른, 회수 가능한 임무 탑재체를 구비한 소형 발사체는, 임무 탑재체와, 상기 임무 탑재체가 적재되는 동체와, 상기 동체의 상부를 덮는 노즈콘을 포함하며, 상기 임무 탑재체에 장착된 회수장치와, 상기 임무 탑재체를 지지하고, 상기 동체의 상하 방향으로 슬라이드 될 수 있는 지지플레이트를 포함하며, 상기 회수장치는, 상기 임무 탑재체에 연결되고, 상기 임무 탑재체에 상대적으로 회전 가능한 회전축, 및 상기 회전축에 방사상으로 연결된 복수 개의 로터를 포함하는 것을 특징으로 한다.


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    Title :

    A small launch vehicle having recoverable mission payloads


    Additional title:

    회수 가능한 임무 탑재체를 구비한 소형 발사체


    Contributors:

    Publication date :

    2023-06-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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