Abstract: The present disclosure relates to a chaff dispensing system that is provided on an aircraft. The chaff dispensing system includes a container, a dispensing assembly, a controller, and a volume of chaff material. The container has a first end, a second end, and a chamber that extends between the first and second ends, and the second end defines an ejection port. The dispensing assembly is provided on the aircraft, and the dispensing assembly is operably engaged to the container. The controller is electrically connected to the dispensing assembly. The volume of chaff material is disposed inside the chamber of the container. The volume of chaff material is dispensed by the dispensing assembly operably through the controller in metered volumes of chaff material. In addition, a first volume of chaff material may be metered at a first time and a second volume chaff material may be metered at a second time in which the second volume of chaff material is different than the first volume of chaff material.

Abstract: A scalable mine deployment system establishes a close range tactical anti-vehicle obstacle. The scalable mine deployment system includes a deployment pod, a munitions control unit and a remote control station. The deployment pod deploys anti-vehicle munitions in response to a control signal received at the remdte control station and relayed via the munitions control unit. The deployment pods are arranged according to desired field properties and are configured to deploy one or more munitions at a selectable density.

Abstract: A tubular body is configured to be disposed around and to apply compression to an extremity. The tubular body includes a treatment area having a first filament and a second filament. Both the first filament and the second filament are disposed to engage the surface of the extremity. The first filament includes AgNP in a concentration effective to promote healing of a wound on the surface of the extremity. The second filament includes a metal having a composition that forms a galvanic couple with silver. The first filament and the second filament are arranged in the tubular body such that the AgNP and metal form galvanic couples across at least a portion of the treatment area when in the presence of a fluid in the wound of the extremity that produce an electric current in an amount effective to further promote healing of the wound.

Abstract: A dispenser unit for countermeasures. A magazine for the countermeasures is removably arranged on the dispenser unit. A dispensing nozzle dispenses the countermeasures out of the magazine. A movable seal is arranged within the magazine. The seal in a first position covers the dispensing nozzle and in a second position opens the dispensing nozzle, such that the countermeasures may be dispensed through the dispensing nozzle when the seal is in the second position.

Abstract: A method for launching counter-measures from a launch opening of a dispenser mounted on an aeroplane. The counter-measures are launched in a direction obliquely forwards and downwards relative to the aeroplane. In order to facilitate launching of counter-measures, a low dynamic pressure is created permanently across the launch opening of the dispenser by a fixed element acting on the air stream. An arrangement for storing and launching counter-measures including an elongate body provided with at least one launch opening used for storing the counter-measures in compartments. The arrangement is designed to be mounted on an aeroplane with the longitudinal direction of the elongate body essentially coinciding with the flight direction of the aeroplane. The counter-measures are connected to a firing control unit for feeding firing signals to the counter-measures. The arrangement is designed to be mounted under the aeroplane.

Abstract: A protection system (10) is proposed which comprises a storage container (1), a transport unit (2), an activation unit (3), an ejection unit (4), a monitoring/control unit (5) and a user unit/interface (6), as well as at least one effect body (7). This system (10) is integrated at the front in a flying carrier (11), and a modular system (10), with the object of positioning spoof measures in a defined manner, in this case by means of the effect body (7). The various effect bodies (7) are preferably activated and initiated in a controlled manner without any physical contact, in the same way as pneumatic or mechanical ejection of these effect bodies (7). The effect bodies (7) are packets without any munitions, and are responsible for the actual effect of the system (10) outside the carrier (11).

Abstract: In accordance with the present invention, there is provided a deployment device that is operative to deploy Special Material (SM) to protect the vehicle when an enemy infrared (IR) threat is present. The deployment device constructed in accordance with the present invention comprises at least one, and preferably a pair of canisters which are each filled or loaded with SM, then factory sealed to prevent oxidation or contamination. Each of the canisters included in the deployment device includes an input shaft which, when rotated, is operative to transmit the rotary motion to each of four threaded rods. The rods have two primary functions, which are to advance a piston thereby preloading the SM within the canister toward the open end thereof, and to turn rotary metering devices which are located at the open end of the canister. The advancing piston maintains consistent compression in the SM stack within the canister.

Abstract: An electrical power disruption device including a projectile configured to be propelled upwardly from a hand-held launcher and receiving a plurality of electrically conductive streamers.

Abstract: A dispenser system for a platform. The dispenser system is configured to be mounted to the platform and connected to power- and control-system of the platform. The dispenser system includes a dispenser for countermeasure boxes. The dispenser is configured for non-pyrotechnic dispensing and opening of the boxes. Each box is sealed by a detachable closure that includes a first opening member and at least one passive, second opening member stationarily fixed to the dispenser, which is provided with a motor gear. The first and second opening members are configured for detaching the closure by mutual interaction simultaneously as each box under the influence of the motor gear is launchable from the dispenser.

Abstract: A dispenser for a platform, configured to be mounted to the platform and connected to power- and control-systems of the platform. The dispenser includes a magazine for a plurality of pyrotechnic countermeasure cartridges. The magazine is configured for removable fixation to the dispenser by one single fixing bolt in a central location thereof for securing the magazine to the dispenser in an operative mode. A first lock associated with the dispenser and a second lock associated with the magazine are configured to arrest the fixing bolt in interlocking engagement with the first lock and preventing the fixing bolt from coming loose due to environmental influence.

Abstract: A method of disrupting electrical power transmission including the steps of launching a projectile from a hand-held launcher, ejecting a plurality of electrically conductive members from the projectile, and bridging electrical contacts of power transmission equipment.

Abstract: A system for launching a countermeasure device is disclosed. In the illustrative embodiment, the system uses an electromagnetic catapult to throw a countermeasure payload, wherein the azimuth, elevation, and propulsive force of the electromagnetic catapult are controllable.

Abstract: A disruptive media dispersal system for aircraft which absorbs and scatters directed energy weapon beams such as tracking lasers and high energy lasers (HELs) is disclosed. The system may include laser detectors, laser beam propagation disruptive media and a dispersal system. When attacked by a directed energy weapon such as a laser, the laser detector system or vehicle operator deploys the disruptive media. The disruptive media is released by a feeder and dispersal system into the air in the path of the tracking and/or HEL weapon. For example, the dispersal system may be located onboard the aircraft near the front of the fuselage.

Abstract: A method for discharging countermeasures, a rocket launcher, and a dispenser arrangement. A space for one or more rockets in a rocket launcher is used as a carrier for a dispenser arrangement for countermeasures. The dispenser arrangement is designed with one or more cylindrical sections specially adapted to the rocket space in the rocket launcher. Equipment already adapted to aircraft can be used in supplementing the countermeasure equipment of the aircraft.

Abstract: A chaff element for interfering with radar signals. The chaff element has a dielectric substrate and a pair of elongate electrically conductive elements, having a total length of approximately one-half wavelength of the radar signals or otherwise tuned to the radar signals, disposed on the dielectric substrate. A switch is arranged to electrically couple the pair of elongate elements together in response to a control signal generated by an oscillator circuit and a battery. The chaff element can be used in a method of providing a countermeasure against radar signals. A plurality of chaff elements can be deployed in an airspace above a radar unit emitting a radar signal and interfere with the radar signal by opening and closing the switches of the chaff elements while deployed in said airspace above the radar unit.

Abstract: An infra-red emitting decoy flare comprising a rupturable container 13 housing combustible flakes 1 and ignition means 20 for igniting the combustible flakes 1. Each of the combustible flakes 1 comprises a fibrous, carbon containing substrate on to which has been vapor deposited on one or both faces thereof a combustible material layer which is capable, in use, of igniting substantially simultaneously the entire surface onto which it is deposited.

Abstract: A method and an arrangement for discharging countermeasures from a carrier craft in the form of an aircraft or equivalent. The countermeasures are intended to be spread initially in the form of unit packs that, after they have left the carrier craft, are to screen the same from missiles approaching is guided by built-in sensors, or other threats. It is especially characteristic of the invention that the unit countermeasure packs are spread from the carrier transversely to the lying direction of the carrier craft.

Abstract: The two-payload decoy device has a square outer case, containing a manifold/delay body assembly, a round payload assembly, and a square payload assembly. The square outer case is closed with an end cap. The manifold/delay body assembly is attached to the round payload assembly, which rests against the square payload assembly. Firing a standard impulse cartridge ignites a booster pellet and delay element in the manifold/delay body assembly. Gases flow through openings in the manifold/delay body assembly and down the corner cavities between the round payload assembly and the square case, pushing the square piston against the square payload, which separates the end cap from the case and ejects the square payload. The delay element burns for a specific time, and then ignites a round payload expulsion charge, which creates gases that push the round piston against the round payload, which dislodges a retaining ring, and ejects the round payload.

Abstract: The invention relates to a method for discharging countermeasure means, a rocket launcher (1), and a dispenser arrangement (10). According to the invention, the space (9) for one or more rockets in a rocket launcher (1) is used as a carrier for a dispenser arrangement (10) for countermeasure means. The dispenser arrangement is designed with one or more cylindrical sections (11, 12.2, 12.5) specially adapated to the rocket space in the rocket launcher. By virtue of the invention, equipment already adapted to aircraft can be made use of in supplementing the countermeasure equipment of the aircraft.

Abstract: The invention relates to a method and an arrangement for discharging countermeasure means from a carrier craft in the form of an aircraft or equivalent. In this connection, the countermeasure means is intended to be spread initially in the form of unit packs (13, 13′ and 20) which, after they have left the carrier craft, are to screen the same (23) from missiles (24) approaching is guided by built-in sensors, or other threats. It is especially characteristic of the invention that the unit countermeasure packs (13, 13′ and 20) are spread from the carrier (2) transversely to the lying direction of the carrier craft.

Abstract: A method of decoying an incoming missile from a target. The method comprises deploying an array of barrels each containing multiple projectiles, determining a position and orientation for a decoy image of the target in relation to the incoming missile, and firing multiple projectiles substantially simultaneously from respective barrels of the array to create the image. Each projectile contains image forming matter.

Abstract: A method for decoying an infrared seeker comprising the steps of providing a plurality of small pyrotechnic pellets, igniting the pellets and dispersing the pellets.

Abstract: A method for protecting an aircraft against a threat that utilizes an infrared sensor includes providing a plurality of dispensable infrared sources transported in an infrared-source dispenser with the aircraft. A set of infrared-emitting properties of the infrared sources is selected responsive to a set of infrared detecting characteristics of the infrared sensor. A modulated pattern of the infrared sources is dispensed from the infrared-source dispenser responsive to at least one of the set of infrared detecting characteristics of the infrared sensor, and a geometric engagement scenario of the aircraft and the threat.

Abstract: A camouflage device includes at least one releasable active material disposed in at least one container to interrupt a line of sight, whereby the container can be deployed as a preventive measure and the active material can be remotely activated, if necessary. The container(s) can be brought to the desired location to be off-loaded by a transport vehicle, such as a truck.

Abstract: A method and associated decoy for offering a phantom target for protecting land, air or water vehicles or the like as a defense against missiles possessing a target seeking head operating in the infrared (IR) or radar (RF) range, or a target seeking head simultaneously or serially operating in both wavelength ranges. An effective mass emitting radiation in the IR range (IR effective mass) based on flares and a mass backscattering RF radiation (RF effective mass) based on dipoles are simultaneously made to take effect in an appropriate position as a phantom target. A ratio of dipole mass to flare mass of approx. 3.4:1 to approx. 6:1 is employed; and flares presenting a descent rate approx. 0.5 to 1.5 m/s higher than that of the dipoles are used.

Abstract: A method of packaging a multiplicity of infrared decoy foils into a canister having an aft end and a drive screw extending therein. The present method allows for the controlled dispensing and dispersal of the decoy foils from within the canister and comprises the initial step of assembling the decoy foils into at least one stack. The stack is advanced into the canister, with a preload being applied to at least a portion of the stack through the use of at least one separator plate cooperatively engaged to the drive screw. The preload applied to the decoy foils is of a force greater than or equal to that required to dispense the decoy foils from the canister.

Abstract: A method of packaging a multiplicity of infrared decoy foils into a canister having an aft end and a drive screw extending therein. The present method allows for the controlled dispensing and dispersal of the decoy foils from within the canister and comprises the initial step of assembling the decoy foils into at least one stack. The stack is advanced into the canister, with a preload being applied to at least a portion of the stack through the use of at least one separator plate cooperatively engaged to the drive screw. The preload applied to the decoy foils is of a force greater than or equal to that required to dispense the decoy foils from the canister.

Abstract: The invention relates to a method of producing a screening smoke which is one-way transparent in the infrared spectrum (780 nm-14.0 &mgr;m) and opaque in the visible spectrum. According to the invention a known pyrotechnic screening smoke which is highly absorbent in the visible spectrum (380 nm-780 nm) is generated in the form of an aerosol, pyrotechnic scattered particles between 10 and 100 &mgr;m in size are simultaneously produced in said aerosol, and the resulting two-component smoke is irradiated by an infrared radiation source (spectrum: 780 nm-14.0 &mgr;m) from the smoke producer side.

Abstract: A method of packaging a multiplicity of infrared decoy foils into a canister having an aft end and a drive screw extending therein. The present method allows for the controlled dispensing and dispersal of the decoy foils from within the canister and comprises the initial step of assembling the decoy foils into at least one stack. The stack is advanced into the canister, with a preload being applied to at least a portion of the stack through the use of at least one separator plate cooperatively engaged to the drive screw. The preload applied to the decoy foils is of a force greater than or equal to that required to dispense the decoy foils from the canister.

Abstract: A method of packaging a multiplicity of infrared decoy foils into a canister having an aft end and a drive screw extending therein. The present method allows for the controlled dispensing and dispersal of the decoy foils from within the canister and comprises the initial step of assembling the decoy foils into at least one stack. The stack is advanced into the canister, with a preload being applied to at least a portion of the stack through the use of at least one separator plate cooperatively engaged to the drive screw. The preload applied to the decoy foils is of a force greater than or equal to that required to dispense the decoy foils from the canister.

Abstract: Disclosed is an aerosol generating device comprising a cartridge containing a propellant. When ignited, propellant gases expand through a diffuser, then through and into a clearing pad and then through and into a filler area, thereby de-agglomerating and fluidizing the filler and increasing pressure until a frangible end seal on the retainer end of the cartridge ruptures and releases the filler as an aerosol cloud. Methods for disseminating an aerosol and for using the device are also disclosed.

Abstract: A method for stacking fibers less than 10 mm long into a cartridge case, including an impregnation stage for fibers arrayed into at least one skein together with a solidifiable material, the skein being solidifiable inside a mold and then, in the solidified state, being cut into at least two slices each of a thickness which is the desired fiber length. Such cartridges are for use as screens or decoys against radar or other detection or guidance systems.

Abstract: An aerosol generating device comprising a casing having a base end and a ainer end, with a firing primer mounted through the base end and extending into a propellant zone which contains a propellant. The firing primer is thereby detonationally connected to the propellant. A diffuser plate is mounted inside of the casing on a side of the propellant zone opposite to the firing primer. A filler area inside of the casing is adjacent to the diffuser on an opposite side to the propellant zone. The filler area contains particles of a powder having interstitial void space between the particles. A frangible end seal is attached to the casing within the retainer end, with the frangible end seal being positioned adjacent to the filler area on an opposite side of the diffuser. When activated, propellant gases expand through the diffuser into the fill area deagglomerating and fluidizing the powder particles and increasing pressure until the end seal ruptures and releases an aerosol cloud.

Abstract: A means for preventing the opening of a chaff muffin upon its entry into air stream of its supersonic-velocity carrier rocket, said means comprising a longitudinal wrapping in addition to the usual circumferential wrapping.

Abstract: An aerial decoy comprising a fuselage having forward and aft ends. Disposed within the fuselage are a plurality of decoy discs. Rotatably connected to the forward end of the fuselage is a ram air turbine which is cooperatively engaged to the decoy discs such that the rotation of the ram air turbine facilitates the dispensation of the decoy discs from the aft end of the fuselage.

Abstract: A 12-gauge emergency radar rescue signal cartridge comprises bundles of high density chaff tuned to I-Band frequencies of 8-10 GH.sub.z and packaged in a projectile housed within a 12-gauge 3.0-3.5 inch magnum shot shell. The projectile is deployed to a desired altitude by a propellant charge contained within the base of the shell. The base propellant ignites a pyrotechnic delay train carried by the projectile which allows the projectile to reach apogee geometry before the chaff material is expelled to form a radar reflecting cloud. The cartridge may also be employed to facilitate radar observation of low altitude wind conditions.

Abstract: A projectile, particularly for nonlethal active components. The projectile has a disintegratable shell with pyrotechnic means. The projectile has two or more shell layers made of explosive foil, each alternating with another shell layer made of supportive foil material, between a radially outer shell layer made of supportive foil material and a radially inner protective shell. The different layers made of explosive foil can be ignited sequentially when viewed radially from the outside to the inside.

Abstract: A method for the self-protection of an aircraft or the like against radar-guided missiles and a self-protection device for use in aircraft and the like against radar-guided missiles, which enables in-flight cutting and dispensing of chaff dipoles of a preselected length into the airstream along the flight path of the aircraft. The device comprises a housing enclosing a motor having a flywheel providing a motor inertia that enables the motor to maintain a substantially constant rotational speed when a load is applied, a magnetic clutch, gearing for rotating a platen roller and a cutter roller, as well as means for controlling the operation of the device, and an exit opening with a spoiler for dispensing the cut dipoles into the airstream.

Abstract: A covert, i.e., no visible light emitted, multispectral day/night target marker is disclosed. The marker emits a signature detectable in the electromagnetic spectrum including visible, near infrared, middle and longwave infrared, and radar regions. The marker is particularly useful for marking of target areas so that they can be easily detected from the ground or the air. The visible spectrum is marked by a white or colored pyrotechnic smoke generant. The near infrared region is marked by near infrared emitting photodiodes encased in a hardened polymeric molding compound. These diodes are only visible through night vision devices (image intensifiers). The middle through the far infrared regions are marked by the heat generated from the combustion of the pyrotechnic smoke generant. The smoke generant is housed in a canister having a highly emissive surface. The radar region is marked using radar chaff. The target marker is configured for use with conventional mortar or rocket delivered flare systems.

Abstract: A multiple squib assembly is provided for use in a chaff deployment system. A method of manufacture is also provided. The assembly of this invention represents an improvement over prior art squib assemblies, such as the BBU48. In preferred embodiments, the assembly comprises a brass base plate, a pair of squibs, a center contact connected to the squibs, and a zener diode connected between one of the squibs and the baseplate. All of those components are retained within a molded rubber or plastic body, which is shaped to hold the components in the desired relative position and to form sealing elements around each of the squibs. A reliable, integral assembly is thus provided using a minimal number of parts and electrical connections. In alternative embodiments, a larger number of squibs may be incorporated into the assembly, and alternative discrimination elements may be employed.

Abstract: The member bearing electromagnetic decoys comprises a sliding member (23 to 27) having an open major face closed by a cover of which an extension projects opposite an opening (21A) in a compartment (21) provided for a pyrotechnic portion. When the pyrotechnic charge there disposed has caused ejection of the decoy-bearing sliding member, and after a given delay, it will act on the extension of the cover in order to remove the latter and thereby release it from the electromagnetic decoys. This ensures that the decoys are deployed at the end of a given delay after ejection of the decoy-bearing member from the aircraft.

Abstract: A projectile is described which consists of a contact head and a screen material canister which may be made of aluminum, attached thereto by bolts and, optionally closed with a cover. Contact rings are arranged on an outer casing of the contact head and are connected via firing leads to a primer capsule which is located in the contact head in a centrally disposed box-shaped charge chamber having a substantially gas-tight screw cover at its base and substantially gas-tight ports for the firing leads, the ports being sealed with a sealing agent.

Abstract: A pyrophoric coating formed by leaching aluminum from an aluminide coated web in which the aluminide coating was formed on or into the web by an exothermic and diffusion reaction of a powder containing aluminum and chromium with or without a transition metal selected from the group consisting of iron, nickel or cobalt and in which the weight ratio of chromium to aluminum is at least 1:50 but no more than about 1:4.

Abstract: Payload delivery of a payload compartment containing a delivery device is initiated by a suitable fusing device which ejects the delivery device from a payload section by firing a gas generator in the section base to propel the delivery device forwardly, thereby shearing retaining pins and ejecting the delivery device from the payload section. The fusing device concurrently fires a time-delayed mechanism leading to a second gas generator in the center of the delivery device. The gas generator ignites after the chaff dispenser is clear of the payload section. The ignition reaction pneumatically blows chaff (e.g. metallized dipoles) out of wrapped bundles, leaving the wrapper bonded to the delivery device and disseminating the chaff in a cloud of hot gas and air turbulently mixed in the wind shear occurring in the wake of the delivery device. The delivery device survives the dispensing and dissemination processes without losing structural integrity. Thus, no harmful debris is ejected into the chaff cloud.

Abstract: Pyrotechnic bomb comprising a body (1) containing a burst charge (2) and flare charges (6) whose dispersion and ignition are ensured during the burst, characterized in that the said body (1) is made at least partially from a pyrotechnic composition.

Abstract: A non-pyrotechnic reusable cartridge for ejecting countermeasures, such as chaff, flares, or other payloads. The cartridge comprises a gas chamber storing a compressed gas and including an ejection mechanism and a countermeasure storage section storing a countermeasure. In one embodiment, the ejection mechanism is a solenoid valve. When an ejection signal is transmitted by the pilot, the solenoid valve opens to allow the compressed, non-flammable gas to be released from the gas chamber and push the countermeasure out of the cartridge at a high rate of speed. Other embodiments use a rupture disk positioned between the ejection section and the countermeasure storage section. When an eject signal is received, the rupture disk is either punctured or melted to allow the compressed gas into the storage section, thus ejecting the countermeasure.

Abstract: Rigid containers held assembled together form a dispenser from which chaff s dispersed by internally generated pressure when it exceeds a predetermined ejection level to displace and remove a sealing cap from a retention position causing rupture of an associated snap-lock, followed by controlled dispersal of the chaff.

Abstract: The present invention falls within the sector of infrared or electrogmagnetic decoys for protecting light aircraft or helicopters. It relates more particularly to pyrotechnic cartridges and to ammuniton comprising racks receiving the cartridges. This invention makes it possible, for the same volume of ammunition, to have a larger number of shots and to carry out the loading of the ammunition simply and quickly. The cartridge (1), consists of a sole (2) fixed to a case (3), in which are accommodated a plurality of assemblies (11) comprising pyrotechnical ejection charges (6), pyromechanical assemblies (7), ignition charges (8), effective charges (9) and the caps (10). The case (3) is provided with a plurality of receptacles and comprises at its base either a blocking device (4) or a gasket which is seated in a groove (41).

Abstract: In the field of infrared or electromagnetic decoys for protecting light aircraft or helicopters, pyrotechnic cartridges and ammunition comprising racks receiving the cartridges are described. Thus it is possible for the same volume of ammunition to have a larger number of shots and to carry out the loading of the ammunition simply and quickly. The cartridge (1) consists of a sole (2) fixed to a case (3), in which are accommodated a plurality of assemblies (11) comprising pyrotechnical ejection charges (6), pyromechanical assemblies (7), ignition charges (8), effective charges (9) and the caps (10). The case (3) is provided with a plurality of receptacles and comprises at its base a blocking device (4). The assemblies (11) are independent and are arranged in parallel in the various receptacles of the case (3); the sole (2) is common to the various receptacles of the case (3) and is provided with electrical fuses.

Abstract: System for clearing both light and heavy obstacles, in which one or more flying metal plates are propelled against heavy obstacles by explosive forces which also expand a folded continous rod member into a curvilinear, generally annular configuration that cuts through light obstacles such as concertina wire in the process of unfolding.