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 electromagnetic mobile active system for fitting in a missile with a detonation-operated magnetic field compressor. The magnetic field compressor has at least one stator coil and at least one armature casing, which is at least partially surrounded by the stator coil and kept at a radial distance. The magnetic field compressor has at least one explosive charge embedded in the armature casing. The magnetic field compressor has at least one power source. For activating the detonation of the explosive charge, a trigger system is provided. The trigger system can be controlled by a pulse of current from the power source, depending on a signal supplied by the missile. A great amount of electrical energy can be generated in the stator coil by the detonation. For the directional radiation of the electrical energy generated by the detonation of the explosive charge, the active system has at least one directional antenna.

An electromagnetic pulse protecting method includes: searching a threat 2 that generates an electromagnetic pulse 2a; and generating plasma 6 in a light-condensed point 4 by condensing a laser beam 5 on a light-condensed point 4 in response to detection of the threat 2. Thus, various protection objects which contain a protection object having an electric opening indispensably can be protected from an attack by the electromagnetic pulse.

A method for neutralizing a threat, include: detecting an oncoming object prima facie aimed at a protected platform. In response to the detecting, classifying the object as an Anti-Tank-Guided Missile (ATGM) threat. In response to said classification, calculating fire characteristics of the interceptor, such that the ATGM threat will fall an Electro-Magnetic-Pulse induced neutralization geometric envelope relative to the interceptor, for achieving a neutralization effect of the threat, and firing said interceptor that is equipped with at least an Electro-Magnetic-Pulse warhead according to the fire characteristics.

A direct action restraining tag apparatus is disclosed for interfering with normal operation of a motor vehicle. An example restraining tag includes a housing having an internal compartment. The example restraining tag also includes a pulse mechanism disposed within the internal compartment. The pulse mechanism includes a transmitter configured to generate one or both of a radio frequency pulse and an electromagnetic pulse having a magnitude sufficient to interfere with normal operation of an electronic control module of a motor vehicle.

A non-lethal, non-impact smart projectile fired from a suitable launcher and equipped with a digital camera, CPU microprocessor and computer vision programming that can recognize a designated target and track a moving target, while moving at high speed. An image dataset of the target stored in memory of the CPU that enables the projectile to recognize a human or small UAV drone in real time within fractions of a second. A steering and braking system comprising several fins/air brakes, controlled by the CPU and MEMS micro-actuators, that enable the projectile to track a moving target or slow the projectile down. A projectile equipped with actuators that dispenses a non-lethal, non-impact payload or payloads as the projectile approaches the target.

An apparatus includes a capsule configured to be launched or carried towards an unmanned aerial vehicle (UAV). The apparatus also includes a directed energy device within or carried by the capsule. The directed energy device includes a first inductor configured to generate an inductive magnetic field that is able to inductively couple into one or more electronics of the UAV in order to disable or destabilize the UAV. The capsule can be configured to be launched towards the UAV and can include a loiter mechanism (such as a rotor, umbrella, or parachute) configured to maintain a position of the capsule or to slow a descent of the capsule after launch. The capsule can also be configured to be carried towards the UAV by a different UAV, and the apparatus can further include a tether coupling the capsule to the different UAV.

A system for detecting and defeating a drone is disclosed which includes a detection antenna array configured to detect the drone and a control signal of the drone in a 360 degree field, the detection antenna array being further configured to detect the directionality of the drone with reference to the most dominant of the control signal of the drone detected by each of a plurality of antennas within the detection antenna array; a neutralization system disposed in communication with the detection antenna array; the neutralization system including a transmission antenna configured to transmit an override signal to the detected drone, an amplifier configured to modulate a gain of the override signal, and a processing device configured to generate the override signal and control transmission of the override signal.

A pulse generator for generating an HPEM pulse includes a Marx generator having a plurality of capacitors that are connected in series between two output poles, providing a Marx voltage between the output poles during operation of the Marx generator. A DS resonator has two input poles and each of the input poles is connected to a respective one of the output poles by a respective supply line. The capacitors are physically disposed along a profile line having two ends at each of which a respective one of the output poles is located. A distance between the output poles is smaller than a longitudinal extent of the Marx generator along the profile line.

A system for facilitating active protection of a target from a threat is provided. The system comprises one or more platforms configured for directing operation of the system, and one or more unmanned aerial vehicles (UAVs) configured to operate in the vicinity of the target, and to facilitate detection and/or neutralizing of the threat. The platform is configured for autonomously detecting and providing instructions for neutralizing the threat, and each of the unmanned aerial vehicles is configured for communicating with the platform.