The disclosed technology regards a reusable, non-pyrotechnic diversionary device having a housing assembly which receives and supports a pressure manifold, activation assembly, and a lighting assembly. The housing assembly includes a vessel, a main chassis, and a transparent lens. Positioned within the main chassis is a pressure manifold which supports a compressed gas source. A puncture pin is provided in the activation assembly, and aligned with the compressed gas source to facilitate puncture of the source. The disclosed technology further regards a reusable, non-pyrotechnic diversionary assembly having a housing assembly and a reloading tool. The reloading tool has an externally threaded inner body with an aperture at its distal end sized to receive the puncture pin, and an outer body sized and internally threaded to rotatably receive a portion of the inner body in its shaft, allowing the inner body to traverse through and from the shaft at its distal end. A threaded interface is provided on the outer body of the reloading tool to align with the first support structure of the pressure manifold. The inner body rotationally translates within the outer body to position the distal end of the inner body relative to the puncture pin and allow it to translate the puncture pin from an active position to a secured position.

Non-lethal payloads including at least one of boron and silicon, at least one fuel, and at least one oxidizer. The non-lethal payload may be a single-component or dual-component payload. Methods of producing the non-lethal payloads are also disclosed.

Non-lethal payloads including at least one of boron and silicon, at least one fuel, and at least one oxidizer. The non-lethal payload may be a single-component or dual-component payload. Methods of producing the non-lethal payloads are also disclosed.

A stun grenade for individual adjustment and situation-dependent adaptation of the number of active masses in situ. A switch mechanism is built into the stun grenade, enabling the simultaneous activation of different chambers inside the stun grenade in order to adjust the effect. The switch mechanism is formed by a tube and peripherally integrated boreholes and grooves. A different number of the chambers in the stun grenade is activated by the switch mechanism, thereby increasing or decreasing the active power.

A stun grenade for individual adjustment and situation-dependent adaptation of the number of active masses in situ. A switch mechanism is built into the stun grenade, enabling the simultaneous activation of different chambers inside the stun grenade in order to adjust the effect. The switch mechanism is formed by a tube and peripherally integrated boreholes and grooves. A different number of the chambers in the stun grenade is activated by the switch mechanism, thereby increasing or decreasing the active power.

Provided is a frangible munitions device optimized for a dome and cylinder that yields fragments having shapes corresponding to a predetermined embossment pattern upon explosive rupture. The embossment pattern includes a first set of inner regular hexagonal embossments formed into the dome and cylinder that are aligned with the axis of the cylinder, and a second set of outer pre-deformed hexagonal shapes that distort to produce regular hexagonal shapes after drawing into the cylinder wall. The second set of shapes are separated by sharp transition regions. The shapes are embossed in a repeated pattern around the hollow cylinder and the dome top. The dome yields a plurality of fragments having shapes corresponding to the first set of inner regular hexagonal embossments upon explosive rupture, while the cylinder yields a plurality of fragments having shapes corresponding to the second set of outer pre-deformed hexagonal embossments upon explosive rupture.

Provided is a frangible munitions device optimized for a dome and cylinder that yields fragments having shapes corresponding to a predetermined embossment pattern upon explosive rupture. The embossment pattern includes a first set of inner regular hexagonal embossments formed into the dome and cylinder that are aligned with the axis of the cylinder, and a second set of outer pre-deformed hexagonal shapes that distort to produce regular hexagonal shapes after drawing into the cylinder wall. The second set of shapes are separated by sharp transition regions. The shapes are embossed in a repeated pattern around the hollow cylinder and the dome top. The dome yields a plurality of fragments having shapes corresponding to the first set of inner regular hexagonal embossments upon explosive rupture, while the cylinder yields a plurality of fragments having shapes corresponding to the second set of outer pre-deformed hexagonal embossments upon explosive rupture.

The Electromagnetic Grenade is a destructive device used to disable Unmanned Ground Vehicles (UGV). The Electromagnetic Grenade is a purpose-built shell/round that utilizes an explosively pumped flux compression generator to create an electromagnetic pulse destructive enough to disable or destroy UGVs and similar military equipment which employ electricity as energy for onboard systems. The electromagnetic grenade includes a standard shell casing, a power source, capacitor bank, a solenoid, and a standard fuse. The casing and size of the shell can be changed to suit the weapon system that will employ the Electromagnetic Grenade. The design can be scaled to work with smaller and larger ordinance which will include small arms, artillery shells, bombs, missiles, rockets, sub-munitions, loitering munitions and similar.

The Electromagnetic Grenade is a destructive device used to disable Unmanned Ground Vehicles (UGV). The Electromagnetic Grenade is a purpose-built shell/round that utilizes an explosively pumped flux compression generator to create an electromagnetic pulse destructive enough to disable or destroy UGVs and similar military equipment which employ electricity as energy for onboard systems. The electromagnetic grenade includes a standard shell casing, a power source, capacitor bank, a solenoid, and a standard fuse. The casing and size of the shell can be changed to suit the weapon system that will employ the Electromagnetic Grenade. The design can be scaled to work with smaller and larger ordinance which will include small arms, artillery shells, bombs, missiles, rockets, sub-munitions, loitering munitions and similar.

An auxiliary catapult device of a grenade contains: a throwing tube, a launch unit, and a trigger unit. The throwing tube includes an outlet, a shoulder, a throwing object, two slots, a through orifice, and a first connection portion, wherein the throwing object has a safety lever. The launch unit includes a piston, a first spring, a piston rod, and a pull bar, wherein the piston has a passing orifice, and the piston rod has a receiving orifice and an engagement portion. The trigger unit includes a seat, a button, two retainers, and two second springs, wherein the seat has an accommodating space, an opening, and a second connection portion. The second connection portion of the seat is connected with the first connection portion of the throwing tube. The button has a notch, and each retainer has a hook and a tilted contact portion.