Abstract: A land vehicle (12) for launching a UAV (14) with a wingspan of more than 2 metres, equipped with one or more turbojet or turboprop engines (16), is provided with a catapult system (26) for the UAV (14), comprising a launch ramp (28) and a mobile assembly (44) for supporting the UAV (14). The mobile assembly is guided by the launch ramp (28) in a launch direction (100) over a length of more than 6 metres, and preferably more than 8 metres. The catapult system (26) comprises at least one linear motor (46) comprising an inductor (48) arranged along the linear path and an armature (50) arranged on the mobile assembly (44) and at least one electrical energy accumulator with one or more supercapacitors (58) for supplying power to the linear motor (46).

Abstract: The invention relates to an assembly (10) comprising a launch motor vehicle (12) and a drone (14), the launch motor vehicle (12) being capable of travelling on a launch track to exceed a given speed threshold relative to a surrounding air mass, the launch motor vehicle (12) being provided with a launch ramp (20) cooperating with the drone (14) to, in a launching position, guide the drone (14) from a starting position in a launch direction to the front of the launch motor vehicle (12). The drone (14) comprises one or more reactors (30) and does not comprise a landing gear.

Abstract: The invention relates to an assembly (10) comprising a launch motor vehicle (12) and a drone (14), the launch motor vehicle (12) being capable of travelling on a launch track to exceed a given speed threshold relative to a surrounding air mass, the launch motor vehicle (12) being provided with a launch ramp (20) cooperating with the drone (14) to, in a launching position, guide the drone (14) from a starting position in a launch direction to the front of the launch motor vehicle (12). The drone (14) comprises one or more reactors (30) and does not comprise a landing gear.

Abstract: The invention relates to an assembly (10) comprising a launch motor vehicle (12) and a drone (14), the launch motor vehicle (12) being capable of travelling on a launch track to exceed a given speed threshold relative to a surrounding air mass, the launch motor vehicle (12) being provided with a launch ramp (20) cooperating with the drone (14) to, in a launching position, guide the drone (14) from a starting position in a launch direction to the front of the launch motor vehicle (12). The drone (14) comprises one or more reactors (30) and does not comprise a landing gear.

Abstract: The present invention relates;—to a drone comprising a fuselage (1) provided with a carrying means (11, 12) capable of allowing a belly-to-ground flight position and an inverted flight position, at least one propulsion means (2), autonomous navigation instruments and an axial compartment (10) forming a recess incorporated into an upper part of the fuselage in order to receive a parachutist (h) in the lying position, avionics provided with programmable control means coupled to the autonomous navigation instruments and means for releasing said parachutist controlled by said avionics, characterised in that said release means are designed and intended to ensure the release of said parachutist in the inverted flight position, and,—to a piece of airborne intervention equipment.