The present invention relates to a reusable launch vehicle, which transports cargo from the ground to a space orbit or outer space, and then returns to the ground so as to be reusable like an aircraft, and, more specifically, to a non-separable fairing opening/closing structure for a reusable launch vehicle, and the reusable launch vehicle comprising same, the structure enabling reuse of even a fairing that is separated from the launch vehicle.
La présente invention concerne un lanceur spatial réutilisable qui transporte une cargaison du sol vers une orbite spatiale ou vers l'espace, puis revient au sol de façon à être réutilisable comme un aéronef, et, plus spécifiquement, une structure d'ouverture/fermeture de coiffe non séparable pour un lanceur spatial réutilisable, et le lanceur spatial réutilisable la comprenant, la structure permettant la réutilisation d'une coiffe même séparée du lanceur spatial.
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.
REUSABLE LAUNCH VEHICLE COMPRISING NON-SEPARABLE FAIRING OPENING/CLOSING STRUCTURE, AND OPERATING METHOD THEREOF
LANCEUR SPATIAL RÉUTILISABLE COMPRENANT UNE STRUCTURE D'OUVERTURE/FERMETURE DE COIFFE NON SÉPARABLE, ET SON PROCÉDÉ DE FONCTIONNEMENT
비분리식 페어링 개폐 구조를 포함하는 재사용 발사체 및 이의 운용 방법
2025-01-30
Patent
Electronic Resource
Korean
IPC: | B64G Raumfahrt , COSMONAUTICS |
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