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 supplying the vehicle, to which the unit is to be connected, the tip of at least some of the free ends being contained in the removal plane.
СИЛОВОЙ БЛОК ДЛЯ АППАРАТА-НОСИТЕЛЯ МНОГОРАЗОВОГО ИСПОЛЬЗОВАНИЯ
2017-08-11
Patent
Electronic Resource
Russian
IPC: | B64G Raumfahrt , COSMONAUTICS |
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