An intelligent munition can position circuitry in a 12 gauge form factor that detects the distance from a target in real-time in order to deploy a parachute to slow the munition to a speed that is conducive to accurate, but non-lethal, deployment of at least one electrode toward the target. The munition can intelligently discharge electrical charge into the target via an electrode to disable the target. The munition may further monitor the target and deliver a subsequent electrical discharge in response to detected target movement.

An intelligent munition can position circuitry in a 12 gauge form factor that detects the distance from a target in real-time in order to deploy a parachute to slow the munition to a speed that is conducive to accurate, but non-lethal, deployment of at least one electrode toward the target. The munition can intelligently discharge electrical charge into the target via an electrode to disable the target. The munition may further monitor the target and deliver a subsequent electrical discharge in response to detected target movement.

According to a first aspect of the present invention, there is provided a munition assembly, arranged to be launched from a gun, the assembly comprising: a carrier for a submunition, the carrier comprising a cavity in which the submunition is located; and a submunition, carried by the carrier in the cavity, the submunition arranged to be controllably expelled from the carrier; the submunition comprising: a submunition explosive charge; and a submunition fuze, wherein: the munition assembly is adapted to be launched, into the air, from a gun barrel, where the submunition is then arranged to be controllably expelled from the carrier and enter a body of water; and the submunition fuze is adapted to trigger the submunition explosive charge under water.

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 intelligent munition can position circuitry in a 12 gauge form factor that detects the distance from a target in real-time in order to deploy a parachute to slow the munition to a speed that is conducive to accurate, but non-lethal, deployment of at least one electrode toward the target. The munition can intelligently discharge electrical charge into the target via an electrode to disable the target. The munition may further monitor the target and deliver a subsequent electrical discharge in response to detected target movement.

An intelligent munition can position circuitry in a 12 gauge form factor that detects the distance from a target in real-time in order to deploy a parachute to slow the munition to a speed that is conducive to accurate, but non-lethal, deployment of at least one electrode toward the target. The munition can intelligently discharge electrical charge into the target via an electrode to disable the target. The munition may further monitor the target and deliver a subsequent electrical discharge in response to detected target movement.

According to an aspect of the invention, there is provided a fuze arming system for a submunition, comprising: a first stage, arranged to detect launch of the submunition and its associated carrier; a second stage, arranged to detect expulsion of the submunition from the carrier, and to at least partially arm a submunition fuze based on such detection; wherein the second stage is unable to at least partially arm the submunition fuze without the first stage detecting launch of the submunition and its associated carrier.

Provided is a rocket for artificial rainfall using an ejection hygroscopic flare, the rocket including: a rocket body configured to descend with a parachute after flight by thrust, and having a hygroscopic flare discharge outlet; a communication module installed in the rocket body, and configured to transmit and receive a launch command and an ejection command with a ground station; an ejection hygroscopic flare installed in the rocket body and filled with cloud seeds and a burning material therein; and a hygroscopic flare ejection device configured to separate and eject the ejection hygroscopic flare from an inside of the rocket body to an outside thereof.

A method and an arrangement for preventing a formation of a hurricane storm and/or dispersing a tropical cyclone storm defining an eye are disclosed. The arrangement is dropped from an aircraft into water in the eye of the storm and includes at least first and second vessels filled with a refrigerant. The first and second vessels are pressure resistant, spherical and sinkable with the first vessel having a first sinking velocity and the second vessel having a second sinking velocity. The first sinking velocity is greater than the second. The first and second vessels have respective first and second opening mechanisms for releasing the refrigerant at pregiven respective depths. The first opening mechanism is configured to open at a first depth and the second opening mechanism is configured to open at a second depth. The first depth is greater than the second depth.

A method and an arrangement for preventing a formation of a hurricane storm and/or dispersing a tropical cyclone storm defining an eye are disclosed. The arrangement is dropped from an aircraft into water in the eye of the storm and includes at least first and second vessels filled with a refrigerant. The first and second vessels are pressure resistant, spherical and sinkable with the first vessel having a first sinking velocity and the second vessel having a second sinking velocity. The first sinking velocity is greater than the second. The first and second vessels have respective first and second opening mechanisms for releasing the refrigerant at pregiven respective depths. The first opening mechanism is configured to open at a first depth and the second opening mechanism is configured to open at a second depth. The first depth is greater than the second depth.