A modular canister is provided for containing a missile for launch. The canister includes a set of four longitudinal assemblies, an electronics module, and a hatch module. The assemblies are attachable to form a rectangular cross-section chamber between fore and aft ends. Each assembly includes a wall extrusion and a corner extrusion. The electronics module connects to the chamber at the breech. The hatch module connects to the chamber at the muzzle. The hatch module includes an aperture cover, a door and a hinge. The door pivots on the hinge between a default closed position and a command open position. The chamber can receive or else launch the missile through the muzzle when the door is in the open position.

A canister for storing and launching a self-propelled projectile comprises: a) an inner layer comprising an aluminum foil; b) a top layer consisting of an injected thermoplastic polymer; and c) optionally, a primer and/or a topcoat.

A canister for storing and launching a self-propelled projectile comprises: a) an inner layer comprising an aluminum foil; b) a top layer consisting of an injected thermoplastic polymer; and c) optionally, a primer and/or a topcoat.

A protection device for a rocket launcher includes a cover with a triplet of openings arranged in angularly equidistant positions so as to allow a passage of the rockets housed in two alternating triplets of rocket housings. An actuation means is designed to rotate the cover between a first position in which the triplet of openings is aligned with the first triplet of openings and a second position in which the triplet of openings is aligned with the second triplet of housings.

A protection device for a rocket launcher includes a cover with a triplet of openings arranged in angularly equidistant positions so as to allow a passage of the rockets housed in two alternating triplets of rocket housings. An actuation means is designed to rotate the cover between a first position in which the triplet of openings is aligned with the first triplet of openings and a second position in which the triplet of openings is aligned with the second triplet of housings.

Disclosed is an ordinance-launching tube, including a rear door and an expulsion circuit between a source of pressurized fluid and the tube, and provided with a unit for closing this circuit having an actuator that can be maneuvered by an operator in order to permit the expulsion, the actuator being associated with a detector for the presence of the rear door in the tube-closing position and with a lock for this rear door in the tube-closing position, which can be actuated via a bolt that the operator can move between a first position preventing expulsion and a second position permitting expulsion when the door is in the closing position and locked. The bolt includes an abutment movable between a position blocking the actuator in position to prevent expulsion, and a position releasing the actuator so that they may be actuated by the operator, and thus permit expulsion.

Disclosed is an ordinance-launching tube, including a rear door and an expulsion circuit between a source of pressurized fluid and the tube, and provided with a unit for closing this circuit having an actuator that can be maneuvered by an operator in order to permit the expulsion, the actuator being associated with a detector for the presence of the rear door in the tube-closing position and with a lock for this rear door in the tube-closing position, which can be actuated via a bolt that the operator can move between a first position preventing expulsion and a second position permitting expulsion when the door is in the closing position and locked. The bolt includes an abutment movable between a position blocking the actuator in position to prevent expulsion, and a position releasing the actuator so that they may be actuated by the operator, and thus permit expulsion.

An aircraft comprising a weapons pod including an enclosure mounted to an outer mold line of the aircraft, and at least one missile rail launcher mounted entirely within and fixed to the enclosure.

A stabilized end cap for covering one end of a common launch tube on a military aircraft is disclosed. The stabilized end cap includes a central body having a portion with a disk-shape configuration. In some cases, the stabilized end cap has a peripheral extension that extends radially outward from the periphery of the central body, and the peripheral extension is provided with an aerodynamic configuration. In other cases, the stabilized end cap has at least one aerodynamic extension extending longitudinally outward from the outside surface of the central body.

A stabilized end cap for covering one end of a common launch tube on a military aircraft is disclosed. The stabilized end cap includes a central body having a portion with a disk-shape configuration. In some cases, the stabilized end cap has a peripheral extension that extends radially outward from the periphery of the central body, and the peripheral extension is provided with an aerodynamic configuration. In other cases, the stabilized end cap has at least one aerodynamic extension extending longitudinally outward from the outside surface of the central body.