Mar 10, 2026
The disclosure relates to a device for providing a ballistic solution. In one embodiment, the disclosure relates to a device for storing one or more ballistic calculators for providing a ballistic solution. In one embodiment, the device communicates with one or more laser rangefinders.
Mar 10, 2026
A mine clearing device configured to be propelled into an area and detonated after landing has a detonating cord and a plurality of explosive blocks along the detonating cord. Each of the plurality of explosive blocks is configured such that, upon landing, a majority of the explosive material is between a ground and a horizontal plane of the detonating cord.
Mar 10, 2026
Projectile guiding assemblies, caps and methods of delivering power for testing and optionally data over spring-mounted fin(s) of the guiding assembly are provided. The guiding assemblies are configured to have continuous electrically conductive path(s) from the fin(s), through the respective spring(s) on which the fin(s) are mounted, and into the electronics module, which may receive power for testing and guiding data from external source(s) over the electrically conductive path(s). In the testing state, cap mechanically secures the fin(s) to contact(s) thereupon to assure continuous power and data transfer, sparing surface area that was previously dedicated to power and data transfer and simplifying these processes, especially under field conditions.
Mar 10, 2026
A guided vehicle that includes a body, a propulsion system operably engaged inside of the body, a housing operably engaged with the body and encasing a guidance device inside of the housing, a viewing window of the guidance device, and a cover moveably engaged with the housing, wherein the cover is moveable between a pre-flight configuration and a flight configuration. In the pre-flight configuration, the cover covers the viewing window. In the flight configuration, the cover is configured to expose the viewing window in the flight configuration in response to an impulse of acceleration generated by a launch of the guided vehicle.
Mar 3, 2026
An armor carrier comprises a plate bag removably attachable to a soft armor carrier. The soft armor carrier comprises at least one panel and, in some cases, a front panel, a rear panel, and a pair of shoulder straps. The pair of shoulder straps may include one or more spaced-apart slit openings in a patterned configuration, and the front and rear panels of the soft armor carrier include one or more spaced-apart slit openings in a horizontal or vertical orientation. The plate bag, which comprises a front panel, a rear panel, and a pair of shoulder straps corresponding with respective components of the soft armor carrier, is donned over the soft armor carrier. The plate bag is removably secured to the soft armor carrier via one or more attachment fittings disposed on the plate bag that respectively engage the one or more of slit openings on the soft armor carrier.
Mar 3, 2026
In a MEFP warhead detonation of the main charge is controlled to provide elevated pressure at multiple locations on the back surface of the liner to cut the liner and to form and propel forward a plurality of EFPs. An initiation system is configured for multi-point initiation of a plurality of booster charges to detonate the main charge to produce a plurality of detonation waves that constructively interfere at multiple locations on the back surface of the liner to form pressure hot spots that cut the liner and to form and propel forward a plurality of EFPs. In different embodiments, the elevated pressures are between 110% and 200% of the detonation pressure at the front of an individual detonation wave. The liner may, for example, be a flat plate or a include a plurality of dimples in which case the boosters are aligned to the center of the dimples.
Mar 3, 2026
A warhead includes a casing having a periphery wall that extends along a central axis from a forward end of the casing to a rearward end of the casing. The casing defines a cavity configured to contain an explosive material, wherein the forward end of the casing includes a first thread pattern configured to engage a guidance system casing, and the rearward end of the casing includes a second thread pattern configured to engage a propulsion system casing. A first row of fragments is arranged along a first section of the periphery wall of the casing. A plurality of second rows of fragments is rearward of the first row of fragments and arranged along a second section of the periphery wall of the casing. In an example, each of the first and second sections tapers inward towards the central axis as it extends toward the forward end of the casing.
Feb 24, 2026
Vacuum insulation layers are provided for one or more components of a launch system for a plurality of missiles. The vacuum insulation layers may be integrated into the walls of the components or provided in inserts attached to the components. A medium or high vacuum is pulled on a sealed void space in the walls or the insert. The vacuum insulation layer provides a thermal conductivity (Tcond_vac) of less than one-third of a thermal conductivity of air (Tcond_air). The vacuum insulation layer delays desensitization or inhibits premature reaction of the energetic materials inside the missiles due to high external temperatures. The insulation layers allow for more compact and dense configurations of the launch system and missiles.
Feb 24, 2026
A portable launcher to launch a guided projectile at an aerial target, wherein the guided projectile has a projectile guidance kit and a target leading guidance kit that is provided with the guided projectile and the portable launcher. The target leading guidance kit includes a target lead estimation protocol stored on a computer readable media and accessible by a processor of the target leading guidance kit. When the processor executes the target lead estimation protocol, the processor is instructed to dynamically lead a reticle of an electronic sight of the target leading guidance kit from the initial target position to the lead target position in response to the projectile guidance kit detecting a speed of the aerial target and an inertial measurement unit of the target leading guidance kit that measures the slew of the guided projectile from the initial position to the translated position.
Feb 24, 2026
A navigation system and method for guiding a vehicle with respect to a source of jamming is disclosed, the system and method being capable of receiving navigation-aid signals, detecting jamming of such signals, mitigating such jamming, determining direction to the source of jamming, and interdicting that source, e.g., a drone gun.
Feb 24, 2026
A protective mantel and accessory hub includes a primary yoke configured to be worn underneath an armor carrier. Sliding attachment points removably connect the armor carrier to the upper protector to allow for mobility and articulation. Accessories such as a throat guard and deltoid guards are removably attached to the mantel. Shoulder suspension members are inserted into the primary yoke to support and distribute the weight of the armor carrier. The armor carrier includes a magnetically attachable front accessory panel and zippered pouches on the front and back to receive and retain body armor plates.
Feb 24, 2026
An EFI or LEEFI provides enhanced detonation energy sufficient to directly detonate a main charge to improve the reliability and ease the qualification of an explosive firing train. This is accomplished by forming the EFI's output charge from an explosive material typically used as a booster explosive (e.g., PBXN-5, CH-6 and Composition A5) rather than a primary explosive and making the diameter of the output charge greater than the diameter of the barrel thus increasing the total mass of the output charge. The explosive firing train now requires only a single explosive transfer interface. For use in military grade munitions, the EFI's casing is formed with one or more vent holes radially adjacent the output charge.
Feb 17, 2026
A method of controlling a gyroscopically-stabilized projectile, comprising a control system producing a control signal, a rotating aerodynamic shell, and a reaction mass system responsive to the control signal, the method comprising: imparting rotational and translational kinetic energy to induce gyroscopic stabilization of the projectile about a gyroscopic axis and a movement of the projectile along a flight path; interacting the shell with surrounding air while moving, to induce aerodynamic forces; generating the control signal from the control system; and altering a state of the reaction wheel system selectively in dependence on the control signal, to alter the flight path.
Feb 17, 2026
A multi-piece ballistic shield is provided with a first shield having an outward face exposed to projectiles and an opposing inward face. The first shield having a first offset layer mechanically coupled to a first section of the outward face of the first shield and a second offset layer mechanically coupled to a second section of the outward face of the first shield. The multi-piece ballistic shield further includes a second shield having an outward face exposed to projectiles and an opposing inward face. The second shield is detachably coupled to the first shield such that the second offset layer overlaps a seam formed between the first and second shields. The multi-piece ballistic shield includes a harness coupled to a fastener to support a weight of the multi-piece ballistic shield.
Feb 10, 2026
A conducted electrical weapon (“CEW”) may distribute deployments from the CEW across a same activation event and across different activation events. The system may distribute deployments based on a deployment list. The deployment list may define a sequential deployment order for a deployment connections of the CEW. The system may determine a next deployment connection and activate the next deployment connection based on the deployment list. The system may update the deployment list responsive to activations of deployment connections such that the deployment list is sequentially maintained between activation events.
Feb 10, 2026
A gas generator includes a housing, an ignition device attached to one end side of the housing, a combustion chamber, a diffuser portion formed on the other end side and including a closed end, an open end, and a side wall positioned between the closed end and the open end, a plurality of gas discharge ports formed in the diffuser portion and including a first gas discharge port having a short distance from the combustion chamber and a second gas discharge port having a long distance from the combustion chamber, and a total opening area of the first gas discharge port and a total opening area of the second gas discharge port are different from each other, and a filter accommodated in the accommodating space, the filter extending from a side of the open end toward a side of the closed end in the diffuser portion.
Feb 10, 2026
Device for interception of incoming ordnance, comprises a dispersion unit to disperse an explosive cloud in an expected path of the incoming ordnance, a proximity detector to detect proximity of the incoming ordnance in relation to the explosive cloud; and an ignition unit associated with said proximity detector that ignites the explosive cloud to disrupt the incoming ordnance.
Feb 10, 2026
A laser weapon countermeasure device is described. The laser weapon countermeasure device comprises a sealed capsule having a filler disposed therein. The filler comprises either: a reflective particulate metal; or a precursor for a reflective metal or reflective metal alloy. The capsule is configured to burst in air such that the filler disperses into an aerosol. A countermeasure launcher and a vehicle comprising a countermeasure launcher are also described.
Feb 3, 2026
A stabilized end cap for covering one end of a common launch tube on a military aircraft is disclosed. The stabilized end cap includes a central body having a portion with a disk-shape configuration. In some cases, the stabilized end cap has a peripheral extension that extends radially outward from the periphery of the central body, and the peripheral extension is provided with an aerodynamic configuration. In other cases, the stabilized end cap has at least one aerodynamic extension extending longitudinally outward from the outside surface of the central body.
