A payload container for providing a horizontal dispersion pattern of sub-projectiles suitable for combatting surface targets is in the form of a cylinder and includes at least two sub-projectiles arranged in a core enclosed by a container wall, wherein the sub-projectiles are linearly disposed. In addition, a projectile and use of the same include at least one payload container or a plurality of sequentially arranged payload containers displaced by a displacement angle relative to each other. The displacement angle is predetermined in such way so that the sub-projectiles are vertically lined at the time when the mechanical force from the carrier shell disappears and the sub-projectiles are spread to the left and to the right, providing a horizontal dispersion pattern.

A munition includes a warhead having a warhead axis and axially opposed first and second warhead ends. The warhead includes: a tubular shock attenuation barrier including an axially extending passage extending from a first barrier end proximate the first warhead end to a second barrier end proximate the second warhead end; an explosive core charge disposed in the passage; an explosive main charge surrounding the shock attenuation barrier; projectiles surrounding the main charge; a core charge detonator; and a main charge detonator. The warhead is configured to be activated in each of a first projection mode and an alternative second projection mode. When the warhead is activated in the first projection mode, the main charge detonator detonates the main charge to thereby forcibly project the projectiles from the warhead with a first set of projection velocities and velocity profile. When the warhead is activated in the second projection mode, the core charge detonator detonates the core charge proximate the first barrier end such that a core charge detonation wave propagates through the passage to the second barrier end and, at the second barrier end, the core charge detonation wave detonates the main charge to thereby forcibly project the projectiles from the warhead with a second set of projection velocities and velocity profile. The second set of projectile velocities and velocity profile is different from the first set of projectile velocities and velocity profile.

A munition includes a warhead having a warhead axis and axially opposed first and second warhead ends. The warhead includes: a tubular shock attenuation barrier including an axially extending passage extending from a first barrier end proximate the first warhead end to a second barrier end proximate the second warhead end; an explosive core charge disposed in the passage; an explosive main charge surrounding the shock attenuation barrier; projectiles surrounding the main charge; a core charge detonator; and a main charge detonator. The warhead is configured to be activated in each of a first projection mode and an alternative second projection mode. When the warhead is activated in the first projection mode, the main charge detonator detonates the main charge to thereby forcibly project the projectiles from the warhead with a first set of projection velocities and velocity profile. When the warhead is activated in the second projection mode, the core charge detonator detonates the core charge proximate the first barrier end such that a core charge detonation wave propagates through the passage to the second barrier end and, at the second barrier end, the core charge detonation wave detonates the main charge to thereby forcibly project the projectiles from the warhead with a second set of projection velocities and velocity profile. The second set of projectile velocities and velocity profile is different from the first set of projectile velocities and velocity profile.

A holding device and method for decreasing the contact-impact event on sub-projectiles when fired from a barrel, cylinder, carrier shell or the like includes a core and at least two legs that at least partially enclose at least one sub-projectile each. When a projectile is fired from a barrel or the like the sub-projectiles load the legs of the device which are deformed and open up and release the sub-projectiles in a controlled manner without tumbling which leads them to hit and penetrate their target with the short-side. A holding device including sub-projectiles and a projectile including the holding device are also provided.

A warhead for damaging an inflight target includes a frame system, a projectile ejection force generator, and a plurality of long rod penetrators (LRPs). The frame system has a frame lengthwise axis. The projectile ejection force generator is operative to generate an ejection force. The LRPs are mounted on the frame system. Each of the LRPs has an LRP lengthwise axis extending substantially parallel to the frame lengthwise axis. The warhead is configured such that the LRPs structurally support the frame system against axial loads on the frame system. The warhead is configured to dispense the LRPs radially outwardly using the ejection force to thereby form a matrix of the LRPs to intersect the target

An orb or body deployable from a launch tube serves as a countermeasures system. Where used, a tow rocket may be used to tow the orb or body to a desired location generally in front of an oncoming threat, and the tow rocket is released. Multiple line tow rockets are then launched from the orb in every direction, each extending a line connected to the orb to define a spherical volume within which the orb and lines operate. Each line may include at least one of sensors for sensing acoustic, magnetic or other disturbances, countermeasures systems including explosives, antenna, and radiating countermeasures transducers. Explosives or transducers may also be mounted in or to the orb. Magnetic, acoustic or electrical signals or the like may be emitted to confuse a threat, and explosives may be triggered when the threat enters the spherical volume defined by the extended lines.

The present invention relates to longitudinally sectioned bullets and methods that pertain to a penetrable projectile structured to be discharged from a firearm and comprising at least two separable and penetrable, non-fused individual longitudinal body sections and at least one exterior binding element, including at the frontal region of said penetrable projectile, that holds the at least two non-fused individual longitudinal body sections together until they rupture inside of a target, thereby causing the penetrable individual longitudinal body sections to separate away from each other inside of the target as the projectile penetrates the target. The penetrable projectile is thus capable of controlled fragmentation against a soft target, and is optionally adapted to deliver at least one supplemental payload to a target to further damage said target.

The present invention relates to longitudinally sectioned bullets and methods that pertain to a penetrable projectile structured to be discharged from a firearm and comprising at least two separable and penetrable, non-fused individual longitudinal body sections and at least one exterior binding element, including at the frontal region of said penetrable projectile, that holds the at least two non-fused individual longitudinal body sections together until they rupture inside of a target, thereby causing the penetrable individual longitudinal body sections to separate away from each other inside of the target as the projectile penetrates the target. The penetrable projectile is thus capable of controlled fragmentation against a soft target, and is optionally adapted to deliver at least one supplemental payload to a target to further damage said target.

A cannon projectile having an elongated body with a plurality of elongated and circumferentially spaced segments. At least one tether is attached to at least one end of the segments to hold the segments together. A deployment device, when activated, enables the segments to deploy radially outwardly into a pattern controlled at least in part by the at least one tether using aerodynamic and inertial forces only.

A cannon projectile having an elongated body with a plurality of elongated and circumferentially spaced segments. At least one tether is attached to at least one end of the segments to hold the segments together. A deployment device, when activated, enables the segments to deploy radially outwardly into a pattern controlled at least in part by the at least one tether using aerodynamic and inertial forces only.