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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0857876 (1992-03-26) |
발명자 / 주소 |
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출원인 / 주소 |
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인용정보 | 피인용 횟수 : 12 인용 특허 : 0 |
An arrangement for controlling the flight of a launch vehicle and a coupled payload, such a spaceplane, from launch to the separation of the payload from the vehicle. The launch vehicle is provided with controllable gimballed rocket engines and optionally with aerodynamic control surfaces, that are
An arrangement for controlling the flight of a launch vehicle and an associated payload as the launch vehicle carries the payload aloft to the point of separation of the payload from the flight vehicle which comprise: a launch vehicle provided with gimballed rocket engines and adapted to carry a pay
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