Airbus Defence and Space Sas

Arianegroup Sas

Airbus Safran Launchers Sas

Samuel Chevrollier

Benjamin Faure

Angélique Santerre

Eugénio Ferreira

Jérôme Bertrand

Yohann Coraboeuf

Christophe Favre

Pascal Mezieres

Robert Abadie-Lahaille

Pierre Parpaite

Robert Abadie-La-Haille

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

A device for mounting and supporting a generally cylindrical or tapered tank, having a main axis X, that includes a pair of first retaining rods for retaining the tank along a vertical axis Z on each of a first and second end of the tank, a second retaining rod for retaining the tank along a horizontal axis Y, perpendicular to the main axis, on the first end of the tank, and a third retaining rod for retaining in a ball-and-socket joint, the means being located around the vertical axis and connected to the second end of the tank.

Device for retaining a tank in an aircraft

Growing community of inventors

Tarbes, France

Samuel Chevrollier