A lightweight energetic weapons pod 2 that integrates to unmanned aerial systems 1 that enables the operator the ability to engage targets without flight degradation. The device utilizes an energetic weapons pod 2 that may be reloaded to support sustained combat operations. The ability of the device to function as intended is based on explosive mitigation compression zones and recoilless configurations that allow drone survivability during detonation events.

A lightweight energetic weapons pod 2 that integrates to unmanned aerial systems 1 that enables the operator the ability to engage targets without flight degradation. The device utilizes an energetic weapons pod 2 that may be reloaded to support sustained combat operations. The ability of the device to function as intended is based on explosive mitigation compression zones and recoilless configurations that allow drone survivability during detonation events.

A damage matrix generating device proposed. The damage matrix may include a memory and a processor configured to control the memory. The processor may acquire warhead fragment data obtained by classifying mass and number of fragments scattering in given directions as a warhead is detonated, and target vulnerable area data obtained by classifying a vulnerable area according to an encounter relationship between a fragment and a target. The processor may also generate a virtual target based on an approach direction of the fragment to each of the grids, the grids dividing a ground plane. The processor may further generate a damage matrix by extracting encounter information of fragments to meet the virtual target as the fragments scatter in the given directions based on the warhead fragment data and calculating a damage probability for each ground location according to the encounter information based on the target vulnerable area data.

The present invention provides a method of making a metal injection molded ammunition cartridge comprising the steps of: providing an ammunition cartridge mold comprising a bottom portion having a primer recess extending into the bottom portion adapted to receive a primer, a flash hole positioned in the primer recess through the bottom surface; side walls extending from the bottom portion to a nose end aperture, wherein a propellant chamber is formed between the nose end aperture and the bottom surface; injecting a metal composition into the ammunition cartridge mold to form a metal injection molded ammunition cartridge; and removing the metal injection molded ammunition cartridge from the ammunition cartridge mold.

In an example, an apparatus includes a cryogenic container configured to store a cryogenic fluid, a superconducting coil disposed within the cryogenic container, and an outer casing surrounding at least a lateral surface area of the cryogenic container. The apparatus is configured such that, while the superconducting coil is carrying a current, is in a superconducting state, and is being cooled by the cryogenic fluid stored in the cryogenic container, an outward magnetic pressure is imposed on the cryogenic container and the outer casing. The cryogenic container and the outer casing are configured to withstand the outward magnetic pressure for at least a predetermined period of time, including while the superconducting coil is being charged to the superconducting state. An occurrence of a trigger event while the outward magnetic pressure is being imposed causes the cryogenic container and the outer casing to expand and burst into radially-dispersed fragments.

The present invention provides a method of making a metal injection molded ammunition cartridge comprising the steps of: providing an ammunition cartridge mold comprising a bottom portion having a primer recess extending into the bottom portion adapted to receive a primer, a flash hole positioned in the primer recess through the bottom surface; side walls extending from the bottom portion to a nose end aperture, wherein a propellant chamber is formed between the nose end aperture and the bottom surface; injecting a metal composition into the ammunition cartridge mold to form a metal injection molded ammunition cartridge; and removing the metal injection molded ammunition cartridge from the ammunition cartridge mold.

An anti-personnel autonomous vehicle (APAV) system has a fuselage formed by a directional fragmentation weapon (DFW). An unmanned aerial vehicle (UAV) assembly is engaged to the DFW, the UAV assembly having a plurality of lift units positioned to provide balanced lift on the DFW. A control module integrated in the UAV assembly has a wireless transmitter/receiver communicating with a remote controller.

In an example, an apparatus includes a cryogenic container configured to store a cryogenic fluid, a superconducting coil disposed within the cryogenic container, and an outer casing surrounding at least a lateral surface area of the cryogenic container. The apparatus is configured such that, while the superconducting coil is carrying a current, is in a superconducting state, and is being cooled by the cryogenic fluid stored in the cryogenic container, an outward magnetic pressure is imposed on the cryogenic container and the outer casing. The cryogenic container and the outer casing are configured to withstand the outward magnetic pressure for at least a predetermined period of time, including while the superconducting coil is being charged to the superconducting state. An occurrence of a trigger event while the outward magnetic pressure is being imposed causes the cryogenic container and the outer casing to expand and burst into radially-dispersed fragments.

A lightweight energetic weapons pod 2 that integrates to unmanned aerial systems 1 that enables the operator the ability to engage targets without flight degradation. The device utilizes an energetic weapons pod 2 that may be reloaded to support sustained combat operations. The ability of the device to function as intended is based on explosive mitigation compression zones and recoilless configurations that allow drone survivability during detonation events.

A lightweight energetic weapons pod 2 that integrates to unmanned aerial systems 1 that enables the operator the ability to engage targets without flight degradation. The device utilizes an energetic weapons pod 2 that may be reloaded to support sustained combat operations. The ability of the device to function as intended is based on explosive mitigation compression zones and recoilless configurations that allow drone survivability during detonation events.