Abstract: It is proposed to combine the cascade effect of frangible pellets with sub-projectiles made of ductile heavy metal, that is, to produce a munition in which the advantages of for example frangible pellets of a central penetrator are combined with the advantages of the ductile heavy metal in an external penetrator\whereby an improved performance on various targets is achieved along with deeper impact speeds.

Abstract: An ammunition cartridge for an electrical discharge weapon having at least one dart positioned within a dart chamber in the housing. The cartridge has at least one adjustable barrel for selection between close and extended ranges and a joint and port for adjusting pressure in the barrel. In another form the cartridge has two fixed barrels and a retractable deflection ramp for selection between close and extended ranges.

Abstract: The present invention relates to decoys for heat-seeking missiles and methods of producing and using the same. The decoys are designed to be kinematic or pseudo-kinematic, producing one or more infra-red radiation emitting clouds that give the appearance of a moving infra-red target in the airspace in which the decoy has been released.

Abstract: A warhead including a hit-to-kill vehicle and a hub about the hit-to-kill vehicle including, packaged therein, a net and a plurality of rods held in a spaced relationship by the net for destroying a target when the net is deployed in the vicinity of the target in case the hit-to-kill vehicle misses the target.

Abstract: A method of destroying a target includes positioning a hit-to-kill vehicle in the trajectory path of a target, and deploying a net including a plurality of rods held in a spaced relationship by the net for destroying the target in case the hit-to-kill vehicle misses the target.

Abstract: A kinetic energy penetrator includes a plurality of penetrator segments, a penetrator segment sleeve for storing the plurality of penetrator segments, and means for moving the plurality of penetrator segments from the penetrator segment sleeve to locations substantially aligned along an axis of attack. A method includes storing a plurality of penetrator segments away from an axis of attack and moving the plurality of penetrator segments to locations substantially aligned along the axis of attack. A vehicle includes a body and a kinetic energy penetrator disposed in a forward portion of the vehicle. The kinetic energy penetrator includes a plurality of penetrator segments, a penetrator segment sleeve for storing the plurality of penetrator segments, and means for moving the plurality of penetrator segments from the penetrator segment sleeve to locations substantially aligned along an axis of attack.

Abstract: A non-lethal cargo projectile comprises a projectile body; a fuze adapter attached to a front of the projectile body; a fuze attached to the fuze adapter; a boattail attached to a rear of the projectile body; a pressure tube extending from the fuze adapter to the boattail; a decelerator and drogue chute disposed aft of the fuze adapter; a flexible line that connects the pressure tube to the decelerator; a center disc disposed aft of the decelerator and drogue chute; a rear disc disposed aft of the center disc, the center disc and the rear disc defining a payload volume therebetween; a second flexible line that connects the rear disc to the boattail; at least one shearable fastener that fastens the projectile body to the fuze adapter; and at least one vent extending from the boattail to the fuze adapter.

Abstract: A personal safety device (10) includes at least one housing containing a quantity of a marking substance (30), an explosive charge (36), and a triggering apparatus (22) which is operative to detonate the explosive charge (36) to propel the marking substance from the housing (H) to mark the area surrounding the device.

Abstract: A net is made from an explosive resistant material such as KEVLAR and is thrown over an explosive-laden device such that the net helps contain the blast force of the explosive-laden device. The net also has a nozzle that is fluid connected to a fire suppressant agent as well as a high density foam, each of which are discharged through the nozzle once the net is thrown over the explosive-laden device, the fire suppressant agent and the high density foam each helping to minimize the blast force of the explosive-laden device. The net can be thrown manually or can be fired from a gun that uses either pneumatic force or a firing cartridge to propel the net at its target.

Abstract: A non-lethal cargo projectile includes a projectile body; a nose cap attached to a front of the projectile body; a boattail attached to a rear of the projectile body; a fin assembly including a boom attached to the boattail; a parachute assembly disposed in a front of the projectile body; a cable connecting the parachute assembly to the boattail; a fuze disposed in the boattail; a first pair of half cylinders disposed in the projectile body behind the parachute assembly; a first circular disc disposed at a front end of the first pair of half cylinders and a second circular disc disposed at a rear end of the first pair of half cylinders; a second pair of half cylinders disposed in the projectile body in front of the first circular disc enclose the parachute assembly; and a payload disposed in a space defined by the first pair of half cylinders and the first and second circular discs.

Abstract: An intercept device for flying objects made of a light-weight, packable structure made of a pliable, tear resistant material that can be expanded to a large web-like structure by means of a deployment device, into the path of a flying weapon. To capture, hold and reduce the velocity of intercepted flying objects, activatable resistance bodies are incorporated into uniformly distributed masses that are connected to the perimeter of the web like structure. Contractable sections of the web, made of cable-like structures, connected to perimeter masses, act as drawstrings upon collision with flying object. This causes closure of the web around the flying object as a result of the mass's inertia and added resistance from deployable resistance structures that place tension on drawstring structures of the web. The flying object is subsequently captured within the web, held secure and it's velocity rapidly reduced.

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: An apparatus and method for firing a projectile in which one part of the projectile rotates and the other part of the projectile does not rotate where is it used for delivering a line. The projectile firing apparatus includes a projectile having a part that rotates and a part that does not rotate, and further a barrel with a bore having spiraled grooves and at least two channels for the nonrotating part of the projectile to travel through when the projectile is fired. A line dragging system is mounted on the front of the barrel and engages to the nonrotating part of the projectile. The line dragging system is made of a wire frame including a cylindrical portion, engaging members, frame sides, and engaging locks. Upon firing the projectile, the rotating part moves through the bore of the barrel while the nonrotating part moves through the channels of the barrel.

Abstract: The present invention relates to a system for launching a charge or projectile (40), characterized in that it comprises:

Abstract: A break line launch energy damper and recoil limiting system for line charges absorbs and dissipates launch energy over time during deployment of line charges. This system limits the amount of recoil energy that can act upon the line charge and allows for linear deployment without recoil that might hinder the effectiveness of the rear lengths of the line charge. An elongate strength member connects the line charge to an inertial drag, such as a parachute and/or container for the line charge. A plurality of lines having different tensile strengths are appropriately connected to sequentially part when their tensile strengths are exceeded to thereby absorb and dissipate energy during deployment of the line charge.

Abstract: A hand-held apparatus for projecting a line across an intermediate span includes a launching tube having one end connected to a source of propellant gas energy for launching a projectile, the other end forming an open muzzle adapted to receive and fire a line deploying projectile. The projectile is releasably attached to one end of the line attached to a source of line connected to the launch tube and containing a supply of line to be payed out during the flight of the projectile. An axially-mounted laser sighting device connected to the launch tube for sighting the tube in on a remote target for the projectile is also provided.

Abstract: A line storage device prevents a line from becoming entangled. A channel formed in a piece of material defines a non-overlapping zigzag pattern. The line is laid in the channel and extends from opposing ends of the piece of material. The material supports the line in the channel until the line attains a threshold tension at which point the piece ruptures sequentially along the zigzag pattern from each opposing end. The channel can be formed in or on one or more surfaces of the piece of material.

Abstract: The present invention provides a viable, practical and useful alternative to conventional metal barbed wire that is both portable and easily deployed and has a long storage shelf life. This alternative is a cost effective alternative to metal barbed wire that is reusable, recyclable and unaffected by climactic conditions. There present invention also provides a means for rapid deployment of a permanent or temporary barrier for situations as varied as repairing a breach in a fenced enclosure or providing a no-cross zone in event of civil disturbance. This means is a self-deploying storage canister for the plastic barbed wire which uses a explosive charge for deployment.

Abstract: A ballistically deployed restraining net system including a cartridge receivable within a barrel, the cartridge having a base and an opposing open end. There is a restraining net packaged in the cartridge and a set of weights attached to the restraining net and packaged within the cartridge between the base of the cartridge and the restraining net. A deployment charge ejects the restraining net and the set of weights out of the barrel and out of the cartridge and a spreader charge deploys the weights after the net and the set of weight exit the cartridge so that the weights overtake the net in flight.

Abstract: The present invention pertains to a device with nonlethal interference active bodies for combating aircraft, which violate or do not heed flight bans, etc., and can be forced to land due to vibrations and interferences in the air current on the aerodynamic surfaces. A series of embodiments are described and depicted in the figures of the drawing.

Abstract: Apparatus for launching a projectile comprising a male launching tube having an attachment end and a discharge end opposite from the attachment end, an energy device having a discharge end and having the capability of producing an instantaneous discharge of gas under high pressure from its discharge end, the attachment end of the male launching tube being connected to the discharge end of the energy device whereby the high pressure gases discharging from the discharge end of the energy device are passed through the male launching tube and out the discharge end thereof, a collar mounted on the male launching tube between the discharge end and the attachment end, and a projectile adapted to be mounted on the male launching tube between the discharge end thereof and the collar whereby, when the energy device discharges gas therefrom under high pressure, the projectile will be launched into ballistic flight, the collar having a port extending radially therethrough to the male launching tube, wherein the male laun

Abstract: A ballistically deployed restraining net system including a projectile, a net packaged in the projectile, a net deployment device for unfurling the net in flight, and a fuze for triggering the net deployment device upon the occurrence of a preestablished criteria such as the impact of the projectile with an object, the expiration of a preestablished time period after launch or upon the projectile reaching a predetermined distance to an object.

Abstract: An electronic projectile (10) for use with a standard cartridge (1). Projectile (10) and cartridge (1) are loaded into standard firearms and fired like a standard bullet. After leaving the barrel of a firearm, plastic sheaths (8L) and (8R) fall away and electrodes (19L) and (19R) extend outward on wires (40L) and (40R). On impact the electrodes penetrate the skin of the target making electrical contact with internal tissue of a target. Within projectile (10) a battery (50) powers internal electronics (30) to charge output capacitors (22) and (24) to high voltage. When the capacitors are fully charged a switch (58) completes the circuit and discharges the capacitors through the target. Switch (58) discharges the capacitors 20 to 100 times per second. These pulses continue for several seconds to incapacitate the target. The polarity of the current is changes once or twice per second to alternate between acidic and basic ions being formed around the electrodes to sterilize the puncture sight.

Abstract: A lanyard retainer for use in a breech loading hydraulic speargun. A projectile is attached to the retainer and the retainer and projectile are inserted into the breech end of the speargun barrel with the retainer sealing the breech end of the barrel. A trigger mechanism on the speargun releases water under pressure into the barrel at the location of the connection between the projectile and the retainer. The projectile separates from the retainer and is ejected out the muzzle end of the barrel while the retainer remains in the barrel. The retainer has a forward spindle portion about which a lanyard is wound. The rear portion of the retainer serves as the breech seal and the shoulder between the spindle and the rear portion prevents the lanyard from unwinding onto the rear portion and helps to prevent operator entanglement with the lanyard. The lanyard is attached between the retainer and the projectile such that the lanyard is payed out through the barrel as the projectile travels to its target.

Abstract: A projectile assembly for use in a breech loading hydraulic speargun. The assembly consists of a dart connected to a plug end. The assembly is inserted into the breech end of the speargun barrel with the plug end sealing the breech end of the barrel. A trigger mechanism on the speargun releases water under pressure into the barrel at the location of the connection between the dart and the plug. The dart separates from the plug and is ejected out the muzzle end of the barrel. A lanyard is attached between the plug remaining in the barrel and the dart and the lanyard is payed out through the barrel as the dart travels to its target. The plug end is removable from the barrel and is made buoyant for convenient retrieval of the dart.

Abstract: Fiber-optic cable is wound on a cylindrical bobbin without adhesive and is situated in the vehicle so that the cable, attached to a relatively stationary control computer station, is pulled freely off of the bobbin as the vehicle, such as a missile or torpedo, travels rapidly away from the station. In one embodiment, a propulsion engine is located within the hollow interior of the bobbin and the cable flows outwardly in a helix around the plume of the engine.

Abstract: A rocket-fired visual signalling apparatus and method includes a rocket, an elongated streamer having a first end portion connected to the rocket and a rocket launcher for launching the rocket so that the rocket pulls the streamer into the air such that when the rocket burns out, the streamer is spread out over the surrounding ground cover to facilitate visibility of the streamer.

Abstract: An intercept device for flying objects is formed of a lightweight, small-volume, packable structure made of a tear-resistant, pliable material, which can be stretched to a large, two-dimensional or three-dimensional expansion by means of a deployment device. To reduce the velocity of the intercepted flying objects, activatable, aerodynamic resistance bodies are incorporated into the structure. To end the intercept procedure, elements are integrated into the structure, which consist of material that can be destroyed from outside by means of high-energy beams and/or chemical reagents, or that destroys itself, or the structure as a whole consists of such material.

Abstract: The invention provides an apparatus for the remote control of missiles or torpedoes launched from a launching container, by means of a cable of which a portion is wound onto a supply reel connected with the launching and of which the other portion is wound onto a supply reel in the missile or the torpedo. The supply reel in the launching container is arranged on the forward end of the container, and the supply reel in the missile or torpedo is arranged on the rearward end of the missile or torpedo. The cable section between the two supply reels, before the launching of the missile or torpedo, is fastened along the major portion of its length on the interior wall of the launching container, by means of a gluing arrangement which consists of a material whose combustion temperature is at least by 800.degree. C. lower than the melting temperature of the optical waveguide, or by means of a flexible clamping arrangement whose holding force can be adjusted.

Abstract: A device for capturing humans or animals, comprises a pair of projectiles each having a forward head and a rear shank. Each shank is semi-cylindrical and offset to one side of its associated head, such that when the projectiles are placed together with their shanks contiguous to each other, the two shanks together form a cylindrical body and the two heads together form a flattened body disposed in a plane perpendicular to a mating plane of the two shanks. A flexible tether interconnects the two projectiles, whereby when the two shanks are disposed contiguous to each other and inserted in the bore of the barrel of a firearm, and the firearm is fired, the two shanks will impart thrust to their respective projectiles along lines of force disposed to one side of a center of gravity of each projectile.

Abstract: A line carrying projectile has an axially elongate hollow projectile rod for muzzle loading within the bore of an associated shotgun and an at least partially transparent container assembly mounted on the forward end of the projectile rod and containing a chemiluminescent flare. The flare is removed from the container and activated by bending after which it is reassembled within the container in its active condition preparatory to firing. A part of the projectile frictionally engages and grips an associated portion of the gun barrel to releasably retain the projectile in a launching position within the gun and regardless of barrel orientation until the projectile is fired from the gun.

Abstract: An unpowered air vehicle, i.e. a glider, which is air-launched from appreciable range, is densely packed with a large area, explosive net. At a pre-determined location, the net is extracted from the glider by a parachute and expanded completely before landing on the surface of the water or land that contains a large field of mines. The explosive material in the net is then detonated, destroying the mines covered by the net. The longitudinal ends of the net are attached to a folding, multi-arm framework designed to expand and thereby spread the net after separation from the glider. The spreading action is initiated by an extraction parachute which pulls the first frame from the air vehicle. The spreading action is completed by the second frame which is coupled to a brake mechanism in the glider that maintains tension throughout the net to complete the spreading of the net.

Abstract: Apparatus and method are provided whereby a single rocket or other projectile can be used to deploy a flexible array such as a net. There is provided to the rocket, via a sleeve and an attached flexible nose cone cap, a pair of pivoted, telescoping arms. The rocket is placed in a launch tube that has guides for the rocket, accommodates the swing arms, and has guides for the tow cables for the net. When the rocket is launched from the launch tube, the arms are swung apart on their single pivot such as with one or more loaded springs. After the arms have been swung out, they are held in place such as by a clam shell catch spring. While or after the spring-loaded arms are spread into place, the telescoped arms are extended such as by triggering a gas generator. Tow cables, one attached to each extreme end of an arm, spread out the net while the rocket is pulling it. Stabilization cables are provided that provide a central point of tow contact and better distribute some loads.

Abstract: A gas propelled line deployment system includes a launch tube, and a bullshaped projectile. The launch tube has a closed end with a gas port formed therein and an open end having a plurality of radially extending threaded apertures. The projectile has two spaced, circumferential grooves adjacent the blunt end thereof, with an O-ring mounted in one of the grooves. The projectile is slidably received in the launch tube with the blunt end adjacent the open end of the tube, i.e. the rounded end facing the close end, so that O-ring forms a gas tight seal adjacent the open tube end. Nylon retainer screws are threadedly received in the threaded apertures so that they engage within the other circumferential groove in the projectile. The line to be deployed is attached to an elastic band which is attached to the blunt end of the projectile. A carbon dioxide gas canister communicates with the gas port to introduce a pressurized gas flow into the tube.

Abstract: A gas-propelled line deployment device is operable for orthogonally deplog two antenna lines to a distance of greater than one hundred feet. The device includes first, second and third tubes, closed at one end and open at one end, the first and second tubes being arranged perpendicular to each other and the third tube being arranged along the resulting vector of the axes of the perpendicular tubes. The first and second tubes have wire-carrying projectiles received therein and the third tube has a recoil piston received therein, said projectiles and piston making a gas tight seal with their respective tube. The recoil piston has a larger cross-sectional area than each of the first and second wire-carrying projectiles. The device further includes a retainer mechanism which is operable for retaining the wire-carrying projectiles and the recoil piston within their respective tubes until a predetermined gas pressure is achieved.

Abstract: The invention relates to a weapon whose main object is to attack targets, such as armoured tanks, from above unexpectedly. The weapon includes an active part (1), a propulsion unit, such as a launching device (2), an anchorage attachment (4) which is intended to be firmly anchored in relation to the terrain, and a line (3) whose first end (5) is attached to the active part (1) and whose second end (6) is pivotally attached to the anchorage attachment (4). When used, the active part (1) is launched vertically upwards, with the line (3) held taut, whereafter the active part is guided by the line through the air in a circular arcuate path or trajectory (8) to a target (7), with the centre of the arcuate trajectory in the anchorage attachment (4).

Abstract: A cable is provided for attacking rotating wing aircraft by breaking and/or fouling rotor blades and/or blade pitch adjusting mechanisms. The cable comprises a stretchable core and shallow helix angle outer strands. A high hysteresis rubber or rubber-like material occupies the spaces between the strands and the core. The high hysteresis material prevents the cable from bouncing off the rotor blades when coming into contact therewith.

Abstract: A shot cartridge is made to contain a projectile system for harmlessly ensnaring a fleeing person. The projectile system employs three or four buckshot paired with an equal number of twinned fish hooks. Each buckshot and fish hook pair is joined by a thin strong line, and all said lines are joined at a single site. The fish hooks are separately housed adjacent the rear of the cartridge. The buckshot are separately housed adjacent the front of the cartridge. The line is housed within the cartridge in a compacted state. When fired, the projectile system deploys with an assured wide pattern.

Abstract: A bola body, a bola, and methods employing such bola bodies and bolas; in one aspect a bola body having a non-spherical body member from which extend one or more fingers for entanglement with a bola line, with each other, or for latching onto part of a target body.

Abstract: A projectile to be fired by a electric ignition defensive projector attached to an object to be defended has a propellant charge and an active charge and ignition devices for igniting the propellant and active charges. The active charge-ignition device is a mechanical ignition device including a firing pin and a firing pin spring. The mechanical ignition device is tensioned and released by a grappling line which is connected to the projector or a part of a projectile which remains in the projector, and is likewise connected to the firing pin. After the projectile has been fired and when it has travelled through a range of fire that corresponds to the length of the grappling line, then the firing pin spring is tensioned by the now taut grappling line and the firing pin is subsequently released which then ignite the active charge of the projector via a percussion cap and a pyrotechnical igniter train.

Abstract: A remote injection device for animals comprises a barrel with a piston slideable within the barrel from an initial retracted position at one end of the barrel forwardly toward the opposed end of the barrel to discharge liquid in an injection action through a needle at the forward end of the barrel. The piston is held in a retracted position by an O-ring on a release member which projects through an O-ring carried on the inside surface of the barrel. The inner diameter of the O-ring on the barrel can be adjusted by axial movement of the pair collars on the inside of the barrel. This adjusts the amount of force necessary to push the release member O-ring through the outer O-ring to release the piston to be moved by spring to the discharge position. The barrel can be mounted either upon an arrow type projectile so the impact forces are sufficient to release the piston upon engaging the animal.

Abstract: A filament dispenser (18) for a missile data link has a bobbin with end flanges (24, 26) fixedly mounted to the missile (86). A shroud (30) is spaced opposite the filament pack for frictionally engaging a ballooning filament (30) during dispensing to reduce ballooning amplitude. A second version passes the dispensed filament back through an opening (38) in the bobbin for reverse dispensing. A third version is similar to the first version and, in addition, on leaving the bobbin filament (48) passes through a relatively small diameter ring (52). In a fourth version, similar to the second version, the filament (80) passes through a constraining ring (82) located within the bobbin opening (38). In a final version the filament dispensed from a pack (92) passes around a curved end flange (90) then back over a curved surface (106) and through an opening (102) forming two balloons (109, 110) and helix elimination.

Abstract: A transport unit for transporting fire fighting hoses, explosive materials, equipment or other items, the unit having a projectile launcher including a pressure tank providing a compressed gas chamber, and a projectile barrel mounted on the tank in fluid communication with the interior of the tank, a projectile positioned in the barrel, a hose or other line connected at one end to the projectile launcher and adapted for connection at its other end to the projectile, the line being adapted for connection to a pressurized fire fighting or explosive fluid source, or the line being comprised of an explosive material, the compressed gas chamber adapted to provide launching force to the projectile upon actuation of the launcher.

Abstract: An optical fiber canister (90) comprises a hollow housing (102) and an optical fiber pack (98) having a plurality of layers of optical fiber (20) supported on an inner surface of the housing (102) with a free end (96) of the optical fiber (20) positioned to pay out from an interior surface of the fiber pack (98). The optical fiber (20) of the optical fiber pack (98) has an amount of adhesive thereon ranging from zero to an amount sufficient to produce a peel force of less than about 2 grams. There is desirably a support layer (110) of a castable elastomeric material between the inner wall (108) of the hollow housing (102) and the outer surface of the optical fiber pack (98), and a release layer of a release material such as polytetrafluoroethylene between the inner surface of the support layer (110) and the outer surface of the optical fiber pack (98).

Abstract: A minefield breaching system or apparatus and a delivery projectile therefor comprises a projectile arranged to be mounted on a rifle, light mortar or similar weapon and to be projected in a desired direction by firing a round from the weapon into the projectile; an explosive line connected directly or indirectly at one end thereof to the projectile; and detonation means arranged to be connected directly or indirectly to the explosive line at the other end thereof for detonation of the explosive line; the projectile comprising a rocket the motor of which is arranged for operational ignition upon a round from the weapon being fired into the projectile, and the projectile carrying a presence or location indicator together with power means for operation of the indicator.

Abstract: A missile data link filament (12) dispenser (10) is located within an enclosure (20) having a single eyelet opening (26) through which the filament feeds on launch. A quantity of a particulate material (28) located within the enclosure (20) is converted to an aerosol mixture by the filament movement on dispense. The aerosol mixture serves to act as a brake on the filament preventing dispense speed exceeding a predetermined desirable maximum.

Abstract: A long, slender thread or filament of a slow-burning substance is metalli, by evaporation, cold-spraying, or the like, with aluminum, zinc or other similar substance. A short length at one end is not metallized but is provided with means for igniting the filament when the chaff is dispensed. A bundle of these filaments are then packed in an impermeable foil envelope and preferably filled with an inert atmosphere. When dispensed, the cloud of slow-burning filaments perform toward infrared search or tracking devices in a manner analogous to the clutter signal created in radars by conventional chaff. At the same time, the metallic coating on the filament acts as a conventional chaff, giving a capability to interfere with either infrared or microwave devices and devices with a combination of infrared and microwave capabilities.

Abstract: A filament (18) dispenser for on board use in an airborne vehicle (10) in which a cylindrical bobbin (20) is rotatively mounted within the vehicle (10) with the axis of rotation normal to the vehicle longitudinal axis. A brake (48) prevents the bobbin (20) from exceeding predetermined rotational speed limits that would cause filament lift-off. A protective covering (44) is placed on a prescribed filament end portion length as reinforcement against startup tension damage to the filament (18).

Abstract: Guided missiles (10) which trail control umbilicals such as optical fibers (20) are launched from an array (16) of launch tubes (14) that point in the same direction. A swing arm (40) extends over the face of the array (16) to capture and move the umbilicals (20) of previously launched missiles (10) away from the portion of the array (16) from which the next missile (10) will be launched, to avoid interference between the launched missile (10) and the exisiting umbilicals (20). As each missile (10) is launched, the swing arm (40) recycles to capture the umbilical (20) of the newly launched missile (10).

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.