Matter and energy are delivered by superimposing multiple quantum wave states such that composite wave amplitudes are maximized at delivery target points and/or minimized at designated intermediate points. One or more target locations are identified for delivery of matter or energy waves, analyzing the medium along the transit path from the emitters, calculating interaction probabilities at each point along the medium, creating a scoring system for optimizing and limiting thresholds of interaction in designated regions; and calculating a combination of wave frequencies, emitter locations and vectors such that quantum interference between the beams optimizes the scoring outcome. The scoring system may be used to reward amplitudes within a specified range over a specified volume of space and penalized if the amplitude falls outside the range. The combined beam may be used for various purposes, including without limitation biological or military target compromise or elimination, electrical energy delivery, etc.

Disclosed are systems and methods of rapidly cooling thermal loads by providing a burst mode cooling system for rapid cooling. The burst mode cooling system may include a complex compound sorber configured to rapidly absorb ammonia. The system may be used to provide pulses of cooling to directed energy systems, such as lasers and other systems that generate bursts of heat in operation.

According to an aspect of the invention, there is provided a weapon system for use on a vehicle, comprising: a control system, the control system configured to, in response to a determination that a line-of-sight from the weapon system to a target of the weapon system is currently, or going to be obscured, trigger an alteration of a configuration of the vehicle such that the line-of-sight to the target is not obscured. Thus, the weapon system can ensure a line-of-sight of the target, allowing it to be successfully engaged.

A system for detecting and neutralizing a target aerial vehicle comprises a counter-attack unmanned aerial vehicle (UAV) comprising a flight body and a flight control system supported about the flight body operable to facilitate flight of the UAV, and an aerial vehicle countermeasure supported by the flight body. The system can comprise an aerial vehicle detection system comprising at least one detection sensor operable to detect a target aerial vehicle while in-flight, and operable to provide command data to the counter-attack UAV to facilitate interception of the target aerial vehicle by the counter-attack UAV. Upon interception of the target aerial vehicle, the counter-attack UAV is operable to disrupt operation of the detected target aerial vehicle with the aerial vehicle capture countermeasure, thereby neutralizing the target aerial vehicle. The counter-attack UAV and systems may be autonomously operated. Associated systems and methods are provided.

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 device and a method of anti-unmanned aerial vehicle based on multi-camera tracking and positioning, including: a bracket, defined a center, a circumference surrounding the center and a central axis passing through the center; at least three cameras, the cameras are evenly distributed and inclined outwardly on the circumference of the bracket, and center lines of view of the cameras forms an inverted cone; a directional antenna, configured to be arranged on the central axis of the bracket; an electromagnetic module, configured to be coupled to the directional antenna; a pan-tilt, connected to the center of the bracket and configured to drive the bracket to rotate; and a control unit, configured to control the pan-tilt to track a target and lock on to the target according to the video image provided by the cameras, such that the electromagnetic module is manipulated to attack the target.

Matter and energy are delivered by superimposing multiple quantum wave states such that composite wave amplitudes are maximized at delivery target points and/or minimized at designated intermediate points. One or more target locations are identified for delivery of matter or energy waves, analyzing the medium along the transit path from the emitters, calculating interaction probabilities at each point along the medium, creating a scoring system for optimizing and limiting thresholds of interaction in designated regions; and calculating a combination of wave frequencies, emitter locations and vectors such that quantum interference between the beams optimizes the scoring outcome. The scoring system may be used to reward amplitudes within a specified range over a specified volume of space and penalized if the amplitude falls outside the range. The combined beam may be used for various purposes, including without limitation biological or military target compromise or elimination, electrical energy delivery, etc.

A laser weapon system is described. Particularly, embodiments describe subsystems of a laser weapon system including those necessary for laser generation, operational control, optical emission, and heat dissipation configured to provide a lightweight unit of reduced dimensions.

Systems, devices, and methods efficiently calculate optimal flight paths for protected entities given terrain data, aircraft position, flight characteristics, and positions of known threat emitters. The systems and methods execute within the mission planning timeline, and the developed processes allow users to retrieve data from the calculations to effectively place an electronic attack platform at the right place and at the right time to be effective. The calculated optimal flight paths are displayed or otherwise visualized in the mission space. Electronic attack jamming capabilities are combined with projected threat emitter performance information in order to obtain optimal geometrical positioning of the electronic attack relative to the threat emitter. Threat emitter system characteristics are combined with electronic attack aircraft capabilities while simultaneously incorporating the position of the protected entity aircraft and rendered to assist the electronic attack aircrew in providing optimal electronic attack capabilities to protect one or more entities.

A flying vehicle is disclosed with a plurality of projectile systems that each contains a projectile for projecting at another flying device. The flying vehicle can include a control system, a flight system in communication with the control system for enabling the flying vehicle to fly, a first projectile system in communication with the control system and a second projectile system in communication with the control system. The control system determines, based on a characteristic of a target flying vehicle, whether to implement a first mode utilizing the first projectile system or a second mode utilizing the second projectile system to capture the target flying vehicle.