The present invention is capable of containing, transporting, and deploying a plurality of kinetic energy impact drones capable of aerial navigation and swarm formations. The apparatus has a circular profile to accommodate fitting within the inherently circular profile of an Unmanned Aerial Vehicles (UAV) fuselage as well as to allow high rate of drone deployment.

A warhead includes a gas generator, a plurality of barrels, and a plurality of projectiles. The warhead is configured to selectively actuate the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels to strike a target.

A warhead includes a gas generator, a plurality of barrels, and a plurality of projectiles. The warhead is configured to selectively actuate the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels to strike a target.

The present invention relates to a drone for collecting and providing image data for bomb damage assessment and an air-to-ground weapon system equipped with the drone. The air-to-ground weapon system includes: a hitting means moving to a bombardment target to hit the bombardment target; and a drone detachably attached to the hitting means.

A warhead includes a gas generator, a plurality of barrels, and a plurality of projectiles. The warhead is configured to selectively actuate the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels to strike a target.

A warhead includes a gas generator, a plurality of barrels, and a plurality of projectiles. The warhead is configured to selectively actuate the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels to strike a target.

The invention relates to a simulated fragmentation grenade that can be rearmed for reuse, comprising a fixed part attached to springs acting on plates that move between an inner position and an outer position, an axial mobile part passing through the fixed part, the axial mobile part being pushed upwards by a spring, and being axially extended in the upper portion by a rod that is rotatably actuated by a mechanism, the rod being attached to a control casing arranged on the outside such that it can move axially and rotationally on a central extension of the body of the grenade, the axial mobile part having retention means for retaining the plates in the inner position, for releasing that retention according to the movement of the axial mobile part.

The invention relates to a simulated fragmentation grenade that can be rearmed for reuse, comprising a fixed part attached to springs acting on plates that move between an inner position and an outer position, an axial mobile part passing through the fixed part, the axial mobile part being pushed upwards by a spring, and being axially extended in the upper portion by a rod that is rotatably actuated by a mechanism, the rod being attached to a control casing arranged on the outside such that it can move axially and rotationally on a central extension of the body of the grenade, the axial mobile part having retention means for retaining the plates in the inner position, for releasing that retention according to the movement of the axial mobile part.

A cannon projectile having an elongated body with a plurality of elongated and circumferentially spaced segments. At least one tether is attached to at least one end of the segments to hold the segments together. A deployment device, when activated, enables the segments to deploy radially outwardly into a pattern controlled at least in part by the at least one tether using aerodynamic and inertial forces only.

A cannon projectile having an elongated body with a plurality of elongated and circumferentially spaced segments. At least one tether is attached to at least one end of the segments to hold the segments together. A deployment device, when activated, enables the segments to deploy radially outwardly into a pattern controlled at least in part by the at least one tether using aerodynamic and inertial forces only.