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.
BLOC PROPULSEUR POUR VÉHICULE DE LANCEMENT RÉUTILISABLE
PROPULSION UNIT FOR REUSABLE LAUNCH VEHICLE
ANTRIEBSEINHEIT FÜR EINE WIEDERVERWENDBARE TRÄGERRAKETE
2017-09-13
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F02K JET-PROPULSION PLANTS , Strahltriebwerke |
UNITE D’ASPIRATION D’AIR POUR UN PROPULSEUR D’UN VEHICULE
European Patent Office | 2024
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