The present invention relates to a reusable projectile which can be reused like an aircraft by returning to the ground after transporting cargo from the ground to a space orbit or a space place and, more specifically, to a non-separable pairing opening and closing structure for a reusable projectile and a reusable projectile including the same, capable of reusing pairing separated from the projectile.

    본 발명은 지상에서 우주궤도 또는 우주공간까지 화물을 운송한 후 지상으로 복귀하여 항공기처럼 재사용이 가능한 재사용 발사체에 관한 것으로, 더욱 상세하게는 발사체에서 분리되는 페어링도 재사용이 가능하도록 한 재사용 발사체 용 비분리식 페어링 개폐 구조 및 이를 포함하는 재사용 발사체에 관한 것이다.


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    Title :

    Reusable Launch Vehicle having Fairing Open-and-Close Mechanism and Operating Method of the Same


    Additional title:

    비분리식 페어링 개폐 구조를 포함하는 재사용 발사체 및 이의 운용 방법


    Contributors:

    Publication date :

    2024-03-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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