A supercavitating cargo round comprises an energetic payload and an electronic payload. The electronic payload includes programmable circuitry suitable for implementing a digital delay of arbitrary length. The supercavitating cargo round is programmable while in a barrel or loader of a weapon.

Systems and methods are described for a cyber-physical vehicle management system generated by an Integrated Secure Device Manager (ISDM) Authority configured to manage licensing and approval of Cyber-Physical Vehicle (CPV)s, a public/private key pair and a unique ID for the Authority, create a self-signed Authority token signed by the private key, send the Authority token to a plurality of ISDM Node device configured to verify Module device authenticity and in communication with the Authority, store, by each Node, the Authority token, and mark, by each Node, the Authority token as trusted.

A cyber-physical vehicle management system may allow for highly reliable and authentic identity management of cyber-physical systems, unforgeable legal interception devices, and robust relay nodes. A cyber-physical vehicle management system may also provide for human and object bi-directional authenticity verification. In some cases, a cyber physical management system may enable a cyber physical vehicle (CPV) detection and intervention system which may be capable or detection, identification, capture, seizure, and immobilization of CPVs. In some embodiments the CPV detection and intervention system includes a geocoding laser subsystem for determining a location of a CPV.

A cyber-physical vehicle management system may allow for highly reliable and authentic identity management of cyber-physical systems, unforgeable legal interception devices, and robust relay nodes. A cyber-physical vehicle management system may also provide for human and object bi-directional authenticity verification. In some cases, a cyber physical management system may enable a cyber physical vehicle (CPV) detection and intervention system which may be capable or detection, identification, capture, seizure, and immobilization of CPVs. In some embodiments the CPV detection and intervention system includes a geocoding laser subsystem for determining a location of a CPV.

The invention relates to a projectile (1, 8, 9) having at least one payload (5) or explosive charge in the projectile body (2, 7, 10), preferably in the medium caliber range, the payload (5) being integrated into the projectile body (2, 7, 10) in the form of a pyrotechnic charge. The payload (5) can preferably be enclosed and sealed by a core (6, 14) which preferably consists of metal or plastic. In an alternative embodiment, the pyrotechnic payload (5) is disposed behind a penetrator (11) in the projectile body (10), the payload (5) thus being located between the penetrator (11) and the projectile body (10).

An apparatus for processing incendiary capsules for the purpose of prescribed burning. The apparatus includes a reciprocating injector tube driven by a crankshaft and a reciprocating mechanical pump driven by a cam. In order to synchronize these reciprocating motions the crankshaft and cam are joined together as a single part. The incendiary spheres exit a hopper and line up in series in a tube which deposits them one by one into a nest. Each individual sphere is punctured in the nest by a needle then injected with reactant. Each sphere is then withdrawn from the nest and dropped through a discharge opening before the next incendiary in line is processed in the same manner.

An apparatus for processing incendiary capsules for the purpose of prescribed burning. The apparatus includes a reciprocating injector tube driven by a crankshaft and a reciprocating mechanical pump driven by a cam. In order to synchronize these reciprocating motions the crankshaft and cam are joined together as a single part. The incendiary spheres exit a hopper and line up in series in a tube which deposits them one by one into a nest. Each individual sphere is punctured in the nest by a needle then injected with reactant. Each sphere is then withdrawn from the nest and dropped through a discharge opening before the next incendiary in line is processed in the same manner.

The present invention provides a method of making a metal injection molded ammunition cartridge comprising the steps of: providing an ammunition cartridge mold comprising a bottom portion having a primer recess extending into the bottom portion adapted to receive a primer, a flash hole positioned in the primer recess through the bottom surface; side walls extending from the bottom portion to a nose end aperture, wherein a propellant chamber is formed between the nose end aperture and the bottom surface; injecting a metal composition into the ammunition cartridge mold to form a metal injection molded ammunition cartridge; and removing the metal injection molded ammunition cartridge from the ammunition cartridge mold.

Warhead (1) comprising a tubular structure with a front region (2), a rear region (3), an outer wall portion (4), an inner wall portion (5) and a central cavity (6), whereby the outer wall portion (4) comprises a multitude of pre-shaped first fracture elements (7) having a non-spherical shape and a multitude of non-cohesive pre-shaped second fracture elements (9) having a spheroidal shape.

Warhead (1) comprising a tubular structure with a front region (2), a rear region (3), an outer wall portion (4), an inner wall portion (5) and a central cavity (6), whereby the outer wall portion (4) comprises a multitude of pre-shaped first fracture elements (7) having a non-spherical shape and a multitude of non-cohesive pre-shaped second fracture elements (9) having a spheroidal shape.