Abstract: A revolving firing pin system is mechanically linked to a screw-block in a breech-loading mortar system, wherein the revolver firing pin assembly rotates on a centerline that is offset from the centerline of the screw-block assembly. When the revolver firing pin assembly is rotated, the firing pin assembly also rotates. However, until the screw-block assembly is locked, the firing pin is in a safety position that is not in line with the primer of the munition loaded into the mortar system. Only when the screw-block is rotated into a locked position does the firing pin align with the primer of the munition to thus be able to strike the primer when the solenoid is electronically actuated.

Abstract: An electromagnetic launcher having a longitudinal axis includes a pair of longitudinally extending rails; a pair of longitudinally extending insulators disposed between the rails; a bore defined by interior surfaces of the rails and the insulators; and a jacket extending around exterior surfaces of the rails and the insulators; wherein the exterior surfaces of the insulators are substantially flat and further wherein a distance between the exterior surfaces of the insulators is substantially equal to or less than a maximum thickness of the rails.

Abstract: A hardened pump laser comprises a hardened pump chamber that combines the functions of a conventional flash lamp and a conventional laser cavity flow tube. The hardened pump chamber comprises a hardened filter tube and electrodes. The electrodes are sealed to the hardened filter tube. A chamber in the hardened filter tube is filled with gas through the electrodes, then sealed. The hardened pump chamber performs the laser pumping function while further performing filtering and diffusion functions.

Abstract: A shaped charge warhead having a longitudinal axis includes a casing; a liner disposed in the casing; an explosive disposed behind the liner; a wave shaper disposed in the explosive, the wave shaper comprising a low reaction rate high blast reactive material; and a detonator disposed adjacent the explosive. Preferably, the wave shaper is symmetrical about the longitudinal axis. The low reaction rate, high-blast material may be, for example, one of powdered silicon or boron and powdered silicon or boron in a plastic matrix.

Abstract: A munition has an external surface. The munition may be of any type. The external surface includes a coating on at least part of it. Coatings may be, for example, paints, tapes, appliqués or other materials. The coating on the munition includes one or more of reflective material, phosphorescent material and fluorescent material. The reflective, phosphorescent and/or fluorescent coatings are applied to the munition prior to its being deployed. The reflective, phosphorescent and/or fluorescent materials in the coatings are visible at a safe distance from the munition and help to identify unexploded ordnance.

Abstract: An apparatus for counting and storing a number of rounds fired from a gun includes a microcomputer; a non-volatile memory connected to the microcomputer; and at least one piezoelectric transducer connected to the microcomputer and mounted on the gun, the at least one piezoelectric transducer comprising a power source that generates power during operation of the gun. The piezoelectric transducer may also sense the firing of the gun.

Abstract: A modular propellant charge for semi-fixed ammunition is disclosed. The propellant charge is disposed within an ammunition cartridge canister, and permits direct access to each charge increment. Further, the propellant charge comprises at least one charge increment comprising a rigid section of a cylindrical solid of rotation, and each charge increment has a length less than the central cavity of said ammunition canister.

Abstract: A supersonic turning vane includes a suction side and a pressure side; the suction side including an expansion turning wall wherein the expansion turning wall creates an expansion fan that projects into the supersonic flow passage to turn supersonic flow into the turning vane; the pressure side comprising a large radius curved surface, the pressure side and the suction side converging to form a throat wherein a shock is formed upstream of the throat, the shock decelerating the supersonic flow to subsonic conditions and the pressure side turning the subsonic flow; the suction side including an outer nozzle expansion wall downstream of the throat, the outer nozzle expansion wall diverging from the pressure side to form an expansion nozzle that expands the subsonic flow to supersonic conditions.

Abstract: A projectile may be used in a boat tail or base bleed configuration. The projectile includes a warhead casing having a nose end and a base end; a payload disposed in the warhead casing; a motor body attached to the base end of the warhead casing and having an igniter disposed therein; a base closure attached to the motor body, an exterior surface of the base closure being tapered to form a boat tail, the base closure and the motor body defining an interior volume; a propellant disposed in the interior volume, the propellant being used for base bleed operation; and a converter attached to the base closure and extending into the interior volume.

Abstract: A finless projectile provides improved ease of use, aerodynamics, muzzle velocity, drag, target, and excursion accuracy, structural integrity, terminal effectiveness and safety, at lower cost. The finless projectile includes a slug, a forward projectile body, an aft projectile body, an obturator, and a pad. The finless projectile is a full bore projectile that defines a hollow core, but does not include a sabot nor does it carry explosives. The finless projectile functions by kinetic energy transfer from the projectile to the target by deforming the target. The center of gravity of the finless projectile is forward of the center of pressure to provide static stability to the finless projectile.

Abstract: A non-lethal projectile carrier includes a base having a plurality of hinges, each hinge including a tab; and a payload case attached to the base, the payload case comprising a plurality of petaloid members, each petaloid member including an opening in a rear surface for insertion of a corresponding tab; wherein upon exiting a gun tube the petaloid members open and fold toward the base. Each petaloid member includes a lip on one edge and an undercut on another edge so that adjacent petaloid members form lap joints. The hinges are defined by zones of small cross-sectional area in the base.

Abstract: An apparatus for packing containers includes a generally rectangular pallet adapter comprising rows and columns of cups, the rows and columns of cups being substantially orthogonal to each other, each cup comprising a lower portion that is generally circular and an upper portion that is generally rectangular, the pallet adapter including side walls located on its perimeter, the side walls extending upward beyond the cups; and a detonation barrier disposed on the pallet adapter, the detonation barrier the detonation barrier comprising internal row partitions, internal column partitions, two end row partitions and two end column partitions, the internal row partitions and end row partitions being substantially orthogonal to the internal column partitions and end column partitions thereby defining rows and columns of rectangular openings.

Abstract: An artillery charge includes a generally cylindrical body with a hollow core; propellant disposed in the body and first energetic material disposed in the hollow core; and a seal disposed over one end of the hollow core, the seal including second energetic material disposed therein. A laser igniter ignites the second energetic material in the seal, thereby providing more reliable ignition of the first energetic material and the propellant. The artillery charge reliably ignites using a lower powered laser than known charges.

Abstract: A projectile comprises a payload portion and an airburst fuze mounted on a rear of the projectile and explosively connected to the payload portion. The airburst fuze comprises an arming and firing electrical circuit including a setback generator; a slider that is movable from a safe position to an armed position, the slider including a detonator attached thereto; a setback lock and a spin lock that lock the slider in the safe position and, in response to a setback acceleration and a spin rate, respectively, unlock the slider; and an actuator that moves the slider to the armed position in response to a first input from the arming and firing electrical circuit; wherein a second input from the arming and firing circuit activates the detonator when the slider is in the armed position.

Abstract: An in-situ plasma cleaning device (PCD) performs an atomic surface cleaning process to remove contaminants and/or to modify the cylindrical surfaces of both the target and substrate. The atomic cleaning process utilizes a plasma generated locally within the in-situ plasma cleaning device with suitable properties to clean both the target and substrate cylindrical surfaces either concurrently or separately. Moreover, the in-situ plasma cleaning device is designed to traverse the length of the target and the substrate cylindrical surfaces during the cleaning process.

Abstract: A rod sleeve made of smart material sleeves and/or steel sleeves with smart material rings surrounds the rod of a kinetic energy projectile. The rod may be made of DU, tungsten, or other material. Smart materials are materials such as nickel-titanium (nitinol) and copper aluminum nickel (CAN) that can be trained to change to one or more particular shapes at predetermined temperatures. The change in shape occurs on a molecular level, almost instantaneously. The rod sleeve can be made all or in part from smart material. The smart material is trained to shrink at cold temperatures and expand at hot temperatures. The sleeve may then be heated and expanded to allow the sleeve to be pressed on the rod. As the sleeve cools, it compresses and provides required support to rod during gun launch of the kinetic energy projectile. The sleeve heats up while traveling down range due to the aero-ballistic heating of the sleeve material. At this higher temperature, the sleeve expands.

Abstract: A machine gun mount is provided for mounting a machine gun in a movable support arm of a helicopter. The mount includes a gun cradle which is detachably connected to the gun and a pintle one end of which is adapted to pivotably mount the pintle, and thus the mount, on the movable support arm. This enables pivoting movement of the gun in a horizontal plane. The pintle is pivotably connected at the opposite end to the cradle so as to permit the cradle, and thus the gun, to be rotated in a vertical plane through 90 degrees between operative and stowed positions. A locking mechanism locks the cradle in the stowed position. A magazine is attached to one side of the cradle while a spent case and link frame and associated catch bag are attached to the opposite side. The magazine includes an inwardly projecting portion disposed below the cradle.

Abstract: A non-lethal ammunition utilizes dense powder ballast and a two-stage firing sequence for launching non-lethal projectiles of a caliber range from approximately 5.56 mm through approximately 40 mm. The non-lethal ammunition comprises a non-lethal cartridge. The non-lethal cartridge comprises a dense powder ballast and one or more non-lethal projectiles. The dense powder ballast is more massive than the non-lethal projectile providing sufficient payload mass to operate the weapon mechanism while launching the non-lethal projectile at velocities compatible with non-lethal applications. A two-stage ignition system fires the non-lethal ammunition and subsequently fires the more massive dense powder ballast. The firing events are separated by a time delay of less than a second. The non-lethal ammunition provides non-lethal projectile capability for semi-automatic and automatic weapons.