AIR VEHICLE FOR LAUNCHING AEROPORT OF A LOAD

摘要

The vehicle has a supporting and dropping unit (14) supporting and dropping a load (12). Two fuselages (16) carry tail empennage elements (30). The tail empennage elements diverge from one another to form a V shaped tail empennage. An aerofoil comprises a central part (18) between the fuselages, and carries the supporting and dropping unit. Two side wings (20) are extended from the fuselages. A measuring unit measures flight conditions e.g. position, of the vehicle along three perpendicular axes passing by center of gravity of the vehicle.