A spaceplane suitable for aeronautical flight comprising a body and a wing defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters disposed under the lower airfoil surface of same and maneuverable between a stowed position and an inclined extended position for aerodynamic braking during the transition from a phase of space flight to a phase of aeronautical flight of the aircraft.
DEVICE FOR CONTROLLING THE SPEED OF A SPACEPLANE DURING THE TRANSITION FROM A PHASE OF SPACE FLIGHT TO A PHASE OF AERONAUTICAL FLIGHT AND ASSOCIATED TRANSITION METHOD
2016-02-25
Patent
Electronic Resource
English
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