The present disclosure relates to a counter measure effector (100) for targeting unmanned aerial vehicles (UAVs), said counter measure effector comprising: at least one antenna (108, 109) for selectively emitting electromagnetic radiation; a telescopic sight (126) comprising an optical system that is transferrable between a first state, in which the optical system has a first appearance, and a second state, in which the optical system has a second appearance that is different from the first appearance, wherein the counter measure effector (100) is configured to set the optical system in its first state, when the at least one antenna is activated, and in its second state, when the at least one antenna is de-activated.

An Unmanned Aerial Vehicle is disclosed. The Unmanned Aerial Vehicle includes a body, rotors attached to the body, one or more sensors, and an electromagnetic pulse transmitter. The electromagnetic pulse transmitter is configured to transmit an EMP and the Unmanned Aerial Vehicle is configured to track a target Unmanned Aerial Vehicle using the one or more sensors and direct the electromagnetic pulse transmitter at the target Unmanned Aerial Vehicle to disrupt the target Unmanned Aerial Vehicle.

A system for adjusting various parameters of an active electronic component based on sensed characteristics of the active electronic component and/or characteristics of the input or output power.

A projectile for use in a shooting application is disclosed. In one embodiment, the projectile includes a base. The projectile also includes a body coupled to the base, wherein the body is hollow and is used to contain a payload material tailored for a specific shooting application. The projectile further includes a threaded tip coupled to the body. The threaded tip has a stem and a threaded portion, and is threaded to body to be removably coupled to the body. The threaded tip is made using a tip material tailored for the specific shooting application.

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 with primer, 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.

A method for operating a mine-sweeping system and corresponding mine-sweeping system, wherein the mine-sweeping system includes at least one drone for detonating sea mines. The drone has at least one magnet element for magnetically detonating the sea mines. The method includes a) translationally moving the at least one drone in the water and b) carrying out a first rotational movement of the drone with respect to a first degree of rotational freedom.

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 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 radiation source for emitting an electromagnetic HPEM microwave pulse contains a microwave generator for generating the pulse. The generator has a generator opening for outputting the pulse. A horn structure is provided for shaping the pulse. The horn structure has an input opening, which is connected to the generator opening and is intended to radiate in the pulse, and an emission opening for emitting the shaped pulse. The generator contains at least two pulse sources for respectively generating a pulse component. The pulse is the sum of the pulse components. A radiation device contains such a radiation source and a control device for triggering the pulse sources in a temporally synchronized manner for the purpose of respectively emitting a pulse component.

An Unmanned Aerial Vehicle is disclosed. The Unmanned Aerial Vehicle includes a body, rotors attached to the body, one or more sensors, and an electromagnetic pulse transmitter. The electromagnetic pulse transmitter is configured to transmit an EMP and the Unmanned Aerial Vehicle is configured to track a target Unmanned Aerial Vehicle using the one or more sensors and direct the electromagnetic pulse transmitter at the target Unmanned Aerial Vehicle to disrupt the target Unmanned Aerial Vehicle.