Airbus Defence and Space Sas

Arianegroup Sas

Airbus Safran Launchers Sas

Benjamin Faure

Angélique Santerre

Eugénio Ferreira

Christophe Chavagnac

Jean Philippe Dutheil

Thierry Pichard

Samuel Chevrollier

Jérôme Bertrand

Yohann Coraboeuf

Fabrice Ruffino

Robert Abadie-La-Haille

Pierre Parpaite

Pascal Mezieres

Christophe Favre

Robert Abadie-Lahaille

A system allowing for the tilting of the rocket motor such that, in the tilted position, the centre of the nozzle is located at least approximately on the neutral orientation axis of said rocket motor.

Orientable rocket-motor system

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

Airplane

Growing community of inventors

Le Bouscat, France

Benjamin Faure