Abstract: A time delay latch device of the arming assembly of a delay fuze which replaces the current system in support of the U.S. Navy Mine Clearing Program. The time delay mechanism is a mechanical run-away escapement having a one-half pound release force that unlatches an 800-pound load. The mechanical force reduction mechanism that makes up the latch device consists of 10 components rather than the existing 31 and a pyrotechnic time delay mechanism consisting of two components in lieu of the existing 14. Hence, the latch device taught herein provides not only the requisite delay and required latch release force but also reduces the total number of components from 44 to 12; thus creating significant cost savings in manufacturing. Time delay latch mechanism is located within the ram shaft that holds the ram shaft spring captive between the ram shafts and housing. The latching mechanism for the ram shaft comprises two ball detents located within the ram shaft and held in place by the housing.

Abstract: A main energetic ingredient filler useful for propellant-based munitions, comprising filler particles having a fine particle size of less than about 10 micrometers diameter and a thin coating of graphite on the filler particles in an amount such that the weight of the graphite is less than about two percent of the weight of the filler particles. Preferred filler particles have a fine particle size of less than about ten micrometers diameter, and most preferred are fillers with a particle size having an average particle diameter ranging from about two to about eight micrometers. The preferred filler is selected from the group consisting of CL-20, TNAZ, NQ, RDX, HMX and mixtures thereof. Most preferred is a filler of CL-20 ground to an average particle diameter of about five to ten micrometers. The preferred amount of graphite comprises about one percent by weight of the filler particles. The filler may be formed into a propellant including a binder and a plasticizer.

Abstract: A segmented, kinetic energy projectile is formed by stacking several liners in a single warhead, for effectively producing a longer penetrator capable of greatly enhancing penetration. Each individual liner forms a separate penetrator, so that the liners are successively fired and allow for a greater overall target penetration. In one embodiment, the flight path of at least one liner is diverted from the flight paths of the other liners, so that the liners could attack several adjacent targets or provide multiple penetrations. The EFP assembly has the additional capability of utilizing a single warhead that incorporates multiple hits mechanisms. The EFP assembly includes multiple liners that are separated by multiple separators. The separators are non-symmetrically disposed relative to each other, in order to divert the liners toward multiple targets. The liners are diverted from a reference trajectory because the separators impart different angles to the liners.

Abstract: A flameless tracer and marker for small munitions and canon caliber projectiles incudes non-toxic, environmentally friendly chemiluminescent materials which are maintained in separate compartments is described. The munitions when fired glow intensely for several minutes and mark a target area upon impact.

Abstract: A muzzle brake vibration absorber for use on a gun barrel is used to store potential energy during gun firing and re-introduce the energy, in part, to the gun barrel out of phase relative to the gun barrel motion. As a result, the deviation of the gun barrel is mitigated to improve the overall accuracy of the gun system. Additionally, the muzzle brake vibration absorber may compliment the functions of a muzzle brake or fuze setting device for the gun system.

Abstract: Dual mode warheads utilizing high-blast explosives (14) and a shaped charge liner (12) and a process for forming such warheads.

Abstract: A container that is a spirally-wound, laminated, and cylindrically shaped is capable of protecting a mortar or other round from a large number of environmental conditions. The laminate material includes a layer of low-density polyethylene (LDPE) heat-bonded to a kraft paper, and is both durable, strong, and moisture-resistant. During the container manufacturing process, multiple layers of the laminate material, augmented by one or more layers of aluminum foil, are wound in a spiral fashion over an interior cylinder of ammunition container board, using conventional tooling and machinery. Layers of the cylinder are bonded to their contiguous neighbors by adhesive. The ends of the containers are sealed with crimped metal end caps, effecting a durable and moisture-resistance seal and giving the cylinder added crush-resistance. The construction of the container requires no high temperature operations, produces no noxious fumes, and does not expose workers to hazardous or toxic materials.

Abstract: The loader assist for mortars allows for the automated loading of ammunition through the muzzle. The invention assists soldiers by transporting the shell into the muzzle from a lower position near the base of the mortar tube thus reducing exposure to enfilade enemy fire and the effects of muzzle blast. The loader assist comprises a frame surrounding the mortar and attached thereto. The frame is supported on pivots mounted to a turntable such that both the invention and mortar move as a unit. A lift device is positioned at the center of the frame and parallel to the mortar axis. A carriage comprising a transfer device is positioned on top of said frame. Said elevator is comprised of two linear actuators which are positioned opposite each other, allowing the jaws on each shuttle to act in pairs with the respective jaws on the other, to grip the shell in two places.

Abstract: A projectile includes an elongated forebody and an aft section secured to the forebody. The aft section includes a pair of fins affixed to an aerodynamic, cylindrical section. The lift generated by the low-drag pair of fins is sufficient to counteract most foreseeable angles of attack to be experienced by the projectile. The aft section further includes a bearing that couples the aft section to the forebody of the projectile and is capable of allowing the aft section to rotate freely about the longitudinal axis of the projectile and independently of the forebody. Thus, during flight the aft section rotates into the maximum lift plane and provides a restoring moment to the projectile, thus providing necessary stability to the projectile while imparting minimum drag.

Abstract: New aza azetidinium sulfate compounds are described which can be intermediates in the preparation of azabicyclobutane.

Abstract: A low impulse firing attachment and companion ammunition for combination gas and recoil operated automatic weapons is comprised of a barrel insert and piston that provide the mechanism for containing the expanding propellant gases produced on firing. Such mechanism provides the required gas pressure at the gas port of the weapon to power the gas system. The barrel insert also allows the use of a sub-caliber piston for the propellant gases to act against. The gas pressure forces the barrel and piston apart, accelerating the recoiling mass rearward to provide recoil operation. The sub-caliber piston allows the use of the relatively high gas port pressure while limiting the peak force transmitted through the adapter. The blank and adapter provide the appropriate gas pressure at the gas port to power the gas system. The adapter also acts as a piston inside the barrel so that the gas pressure forces the barrel rearward, which provides the recoil operation.

Abstract: A guidance device for projectiles has stationary canards (40) and thrusters (50) positioned on the nose (20) of the projectile (10). The thrusters (50) are initiated from remote or local sensor to provide flight maneuverability to a target.

Abstract: A safe-and-arm device for a projectile fired from a smooth bore gun has a rotor that rotates between a safe position and armed position. A setback sensor retains the rotor in the safe position until an acceleration of the projectile causes the setback sensor to be repositioned. Once the setback sensor is repositioned, a bore rider is released and a rotor spring rotates the rotor to arm the projectile.

Abstract: The present invention uses aerodynamic heating caused by air-friction during flight of a training projectile. The training projectile includes a nose, a body and a tail section. The body has a forwardmost end secured to the nose, and a rearwardmost end secured to the tail. Air friction during flight causes deployment of “passive” shape memory alloy (SMA) aerodynamic members in an assembly to induce drag of the training projectile thereby limiting an effective range of the projectile.

Abstract: A system for sealing an indexing primer magazine and breech assembly of a barrel-type firearm to contain exhaust gases with the flow passage transfers the increased pressure into a sealing force between the insert and indexing primer magazine. Additionally, component parts of the seal are located out of the direct path of the formed exhaust gases to increase system longevity and safety. A seal is located within a recess of either the insert or indexing primer magazine, that is separated from the flow passage for the hot combustion gases from the primer or propellant charge.

Abstract: A monitor device for monitoring the activity of an individual to provide an alarm for anomalous by the individual. The device includes a triaxial accelerometer adapted to measure simultaneously measure acceleration in three orthogonal, linear axes and generate a voltage output identifying the amplitude and frequency of detected motion by the individual in each axis. Also included is interface electronics for receiving the voltage outputs and buffering the voltage outputs to generate a first reference voltage for each axis of the accelerometer. Amplifier electronics amplifies each voltage output and compares each voltage output to the first reference voltage to produce a digital signal. A microcontroller receives the digital signal to compare it to an adjustable second reference voltage.

Abstract: A fuze operates in two modes. In a primary mode, the fuze functions similarly to a conventional M223 fuze. In a secondary, self-destruct mode, a pyrotechnic delay mechanism is initiated. The slide assembly is comprised of an aerodynamic safety release, a safety pin, a rotational firing pin fitted with a resilient member such as a spring, a M55 detonator, pyrotechnic initiator, a pyrotechnic delay mix and end cap. In use, the fuze is fitted to a grenade. As the grenade is dispensed from its carrier, a grenade stabilizer starts to oscillate. The oscillation results in an arming screw and an inertial weight to back out from a slide assembly, allowing the slide assembly to move to an in-line position relative to a main M55 detonator in-line with the arming screw (firing pin). Concurrently, the aerodynamic safety release is lifted in the upward direction under the force of the airstream, releasing the safety pin.

Abstract: This low impulse payload cartridge for automatic weapons includes a case, a piston, an ogive, a payload cup, a payload, and a link. The payload cup and payload is seated into the forward portion of the piston. Gas passages permit propellant gases to bleed into the cavity behind the payload and to accelerate the payload upon firing. An alternative to using bleed gases is to use a separate propelling charge behind the payload. The case and piston are assembled and telescopically secured by means of a crimp or other similar feature, to allow relative movement therebetween during chambering and firing. The link may be allowed to move for some portion of the required relative travel between the link and the base of the case. A shoulder on the piston provides a stop through which reaction loads are transmitted to the rear of the barrel during chambering and firing. The piston telescopes over the case during chambering to provide the relative movement between the link and the case base required for weapon function.

Abstract: A bipod support apparatus for an indirect fire weapon such as the 120 mm mortar comprised of a 55 degree ramp and a longer travel distance between the low, middle and high positions which allows for the mounting of the bipods buffer mechanism to the 120 mm mortar tube to stay in one location at 15.54 inches from the muzzle end of the mortar tube, throughout all the adjustment positions and elevation ranges (800 mils to 1512 mils). The three positions, in lieu of the current two position system, eliminate the constant changing of elevation adjustment positions. The new elevating support assembly with its new guide assembly allows for a smooth motion/transition between the three positions of the main base assembly. A new locking mechanism rotates a quarter turn (90°) to lock or unlock the elevating support assembly. Such lock or unlock action now only requires a one hand operation to unlock-lift-lock the elevating support assembly.

Abstract: A first embodiment of the invention comprises a miniature release and latch anchor assembly that can be fabricated in combination with other moving and fixed elements on a single substrate (3). Such a release and latch anchor assembly has many applications in MEMS-type devices, particularly devices whose moving elements react in response to predetermined inertial loading inputs externally imposed thereupon. This embodiment provides ways of imposing or enforcing sequential operations of moving parts in a MEMS-type device, a necessary operational requirement for safety and proper arming of projected munitions. A second embodiment of the invention is a variation of the first embodiment wherein a reinsertable-re-releasable latch anchor assembly mechanism has insertable anchor feet members (5) in cooperation with the linchpin member (7) whereby re-latching of the anchor assembly can occur.