An electric power generator for a projectile moving through the air is based on vibrational, rather than rotational motion. The electric power generator uses an air stream through, which the projectile is traveling typically 100-250 m/s for mortars to up to 1,500 m/s for sabot or even higher electrically fired rounds. A typical 223 rifle round after being fired has energy of over 1700 J, which is equivalent to 1700 W seconds. If a Nano computer was able to extract energy of for example 50 nanowatts during bullet flight which rarely exceeds two seconds the power needed during the flight would be only a few parts per billion of the bullets energy. Even allowing for very inefficient extraction of power, the necessary power to operate on onboard electronic devices such as computers and sensors can be extracted from the airstream through which the projectile travels.

An apparatus, system, and method for deployment of an electronic warfare (EW) asset are provided. The system includes a projectile launching device capable of launching a projectile round. An EW asset is detachably carried by the projectile round. A deployable parachute is attached to the EW asset, wherein the EW asset is configured to be suspended from the parachute when the EW asset is detached from the projectile round. The related method is used for suppression or obscuration of enemy counterfire radar (CFR) system by initiating an EW effect by the EW asset as the EW asset floats towards a ground surface.

A projectile for firearms comprises a body defining a generally cylindrical base portion opposite an ogive. The body further defines a longitudinal axis. A plurality of pairs of adjacent flutes are defined in the ogive. Each flute has a radius of curvature which decreases along the longitudinal axis from a leading edge to a trailing edge of the flute. The adjacent flutes of each pair define and are substantially symmetrical about a central ridge. Each ridge is coplanar with the longitudinal axis and has a lesser depth than a bottom surface of each flute relative to a curved outer surface of the ogive. Each ridge has a radius of curvature which decreases along the longitudinal axis from an origin to a terminus of the ridge. The decreasing radius of curvature of the flutes prevents the projectile from over penetrating human-sized soft tissue targets without sacrificing energy transfer to such targets.

A cartridge assembly that includes a non-lethal projectile and a carrier configured for retaining and launching the non-lethal projectile. The carrier includes a housing including a combustion chamber, at least one escape aperture, a primer, and a case connected to the housing. The case encases the non-lethal projectile. The case and the housing collectively define a launch chamber that is fluidly connected to the at least one escape aperture. The launch chamber is configured for launching the non-lethal projectile out of the case. The at least one escape aperture is configured for metering pressurized gas from the combustion chamber to the launch chamber for launching the non-lethal projectile.

A propellant driven disrupter (PDD) for disrupting an explosive target, comprising: a disrupter barrel having a breech and muzzle end; a projectile liquid or gas positioned in the barrel and extending a longitudinal distance in the disrupter barrel. The projectile liquid distal end is located farthest from the disrupter barrel breech end. A jet stabilizing projectile (JSP) is at least partially positioned in the barrel and operably contacts the projectile liquid distal end. The JSP has a JSP proximal end facing toward the disrupter barrel breech end and a distal end opposed to the JSP proximal end, wherein some or all of the JSP is positioned in the barrel. The PDD may contain the JSP, with an air region between the JSP distal end and the muzzle end, or an air region in an adapter that is connected to the muzzle end. Also provided are JSP's having improved flight stability for use with liquid or air-filled disrupters and methods of disrupting a target.

Apparatus for inhibiting rotation of a projectile tip relative to a longitudinal axis of the projectile. The projectile includes a tip and a jacket with a core. The tip includes a stem that protrudes into said core. The stem includes a plurality of grooves that engage the core. At least one transverse groove inhibits linear motion of the tip along a longitudinal axis of the projectile. At least one longitudinal groove extending along a portion of the length of the tip stem inhibits rotation about the longitudinal axis. In one embodiment, three longitudinal grooves have a spiral shape with the grooves equally spaced about the circumference of the tip stem. In another embodiment, two sets of longitudinal grooves spiral in opposite directions around the tip stem.

A uniform projectile casing which is utilized for projectiles with different ranges. A projectile of relatively short range can in this case be optimized with regard to payload, whereas a projectile with the relatively long range is subjected to a range optimization, with a reduction in payload. The payload of a projectile of relatively long range is generally lower in relation to a projectile with relatively short range. The artillery projectiles have a projectile casing of equal size for the projectiles of different range. To create an artillery projectile, for example 155 mm, a uniform payload-optimized 30 km projectile casing) is used, from which 40 km projectiles can be generated (produced, assembled) by means of a reduction in payload. The range is selected and defined by mutually different projectile bases. The artillery projectile has multiple modular parts which are assembled in order to create the artillery projectile.

A compressive structural element including: an enclosure having a top, a bottom, and inner wall and an outer wall, a first cavity defined between the inner and outer walls and a second cavity defined by the inner wall; and a non-compressible material disposed in the first cavity; wherein the outer wall has at least a portion thereof inwardly shaped toward the first cavity and the inner wall has at least a portion outwardly shaped towards the first cavity such that a first compressive force acting on the top and/or bottom tending to compress the element by a first deflection causes an amplified second deflection, relative to the first deflection, of the inner and/or outer walls into the non-compressible material, thereby exerting a second compressive force against the non-compressible material, resulting in a resistance to the first deflection and the first compressive force tending to compress the element.

A projectile has a base, a tip, and a body axis intersecting the base at a trailing axis point and the tip at a leading axis point. The projectile includes a meplat that is substantially orthogonal to the body axis and a plurality of standoffs that extend away from both the trailing axis point and the leading axis point.

A projectile has a base, a tip, and a body axis intersecting the base at a trailing axis point and the tip at a leading axis point. The projectile includes a meplat that is substantially orthogonal to the body axis and a plurality of standoffs that extend away from both the trailing axis point and the leading axis point.