F42B12/62

Drone deployment apparatus for accommodating aircraft fuselages
10578398 · 2020-03-03 · ·

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.

LONG RANGE LARGE CALIBER FRANGIBLE ROUND FOR DEFENDING AGAINST UAVS
20200033104 · 2020-01-30 · ·

The present invention is directed to a projectile configured to provide a submunition payload across a wide impact pattern, similar to that of a shotgun, at a range typically beyond the capability of standard shotgun rounds. The additional range is provided in some embodiments of the invention by allowing the tailoring deployment range of the submunition payload based upon a given threat.

Medium caliber high kinetic energy round with tracer and self-destruct mechanism

A medium caliber high kinetic energy round with tracer and self-destruct mechanism having an optimized kinetic energy projectile incorporating a fully hardened projectile body and an explosive self-destruct mechanism for a medium caliber high rate of fire round. The medium caliber high kinetic energy ammunition round incorporates a multiple piece sub-projectile that integrates a tracer and high explosive self-destruct mechanism to neutralize the penetrator during self-destruct and minimize collateral damage during firing.

Medium caliber high kinetic energy round with tracer and self-destruct mechanism

A medium caliber high kinetic energy round with tracer and self-destruct mechanism having an optimized kinetic energy projectile incorporating a fully hardened projectile body and an explosive self-destruct mechanism for a medium caliber high rate of fire round. The medium caliber high kinetic energy ammunition round incorporates a multiple piece sub-projectile that integrates a tracer and high explosive self-destruct mechanism to neutralize the penetrator during self-destruct and minimize collateral damage during firing.

Reconnaissance and communication assembly

According to a first aspect of the present invention, there is provided a reconnaissance and communication assembly, adapted to be launched from a gun barrel into the air. The assembly comprises a carrier (with a cavity) and a payload (within the cavity). The payload is arranged to be controllably expelled from the carrier and once expelled from the carrier, the payload transmits a signal.

Anti-drone firework device

A counter-swarm firework includes a shell casing, multiple streamers positioned in the shell casing, a burst charge positioned in the shell casing and configured to disperse the multiple streamers from the shell casing when discharged, a pusher plate positioned in the shell casing between the burst charge and the multiple streamers, a fire suppressant layer positioned between the burst charge and the pusher plate, and a kick charge configured to launch the shell casing and its contents prior to discharging the burst charge. The fire suppression layer may be configured to suppress heat generated by the discharge of the burst charge.

Long range large caliber frangible round for defending against UAV'S

The present invention is directed to a projectile configured to provide a submunition payload across a wide impact pattern, similar to that of a shotgun, at a range typically beyond the capability of standard shotgun rounds. The additional range is provided in some embodiments of the invention by allowing the tailoring deployment range of the submunition payload based upon a given threat.

LONG RANGE LARGE CALIBER FRANGIBLE ROUND FOR DEFENDING AGAINST UAVS
20190301844 · 2019-10-03 · ·

The present invention is directed to a projectile configured to provide a submunition payload across a wide impact pattern, similar to that of a shotgun, at a range typically beyond the capability of standard shotgun rounds. The additional range is provided in some embodiments of the invention by allowing the tailoring deployment range of the submunition payload based upon a given threat.

Projectile, and warhead assembly and deployment system therfor

A warhead assembly is provided for a projectile includes a forward module having a precursor warhead, and an aft module including a main warhead. The warhead assembly includes a deployment system for selectively deploying the warhead assembly from a retracted configuration to a deployed configuration, at predetermined conditions, to thereby provide a longitudinal displacement between the forward module and the aft module. The deployment system includes an expansion member accommodated between the forward module and the aft module, and configured for being longitudinally expanded under the predetermined conditions to thereby increase a longitudinal dimension of the expansion member and thereby urge the forward module and the aft module away from one another to provide said longitudinal displacement. A corresponding deployment system and projectile are also provided.

Reconnaissance and communication assembly

According to a first aspect of the present invention, there is provided a reconnaissance and communication assembly, adapted to be launched from a gun barrel into the air over a body of water. The assembly comprises a carrier (with a cavity) and a payload (within the cavity). The payload is arranged to be controllably expelled from the carrier and once expelled from the carrier, the payload is adapted to enter the water; and the payload transmits a signal after entering the water.