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|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64G-001/00 B64G-001/40 B64G-001/14 B64G-005/00 F02K-009/97 B64F-005/50 B64G-001/64|
|우선권정보||FR-13 56695 (2013-07-08)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 39|
The invention relates to a propulsion unit for a reusable launch vehicle including a rocket engine supported by a cradle. According to the invention, the cradle includes at least three attachment elements for assembling the unit on the structure of the vehicle to which the unit is to be connected, the at least three attachment elements defining a plane for removing the unit, and in which the unit includes one or more fluid and/or electric links of the engine, each one of the links including a free end to be assembled with a corresponding circuit for supp...
1. A thrust unit for a reusable launch vehicle comprising a rocket engine supported by a cradle, wherein: said cradle comprises at least three fixing members for the assembly of said thrust unit on a structure of said reusable launch vehicle;said at least three fixing members defining a plane for dismantling said thrust unit; andsaid thrust unit further comprises one or more links, the one or more links comprising one or more of fluid links and electrical links, of said rocket engine, each of the one or more links comprising a free end configured for cou...