Abstract:
A method for destruction of hostile projectiles and a design of a low velocity cannon firing projectiles that contain directional ammunition. The method includes: firing from a low velocity cannon at least one projectile containing directional ammunition and detonating this directional ammunition at the optimal distance away from the target.
Abstract:
A method for attacking a target, the method including first, deploying a plurality of projectiles in the trajectory path of the target, and second, positioning a blast fragmentation warhead proximate the target and initiating the blast fragmentation warhead so that any portions of the target which survive the blast fragmentation warhead are destroyed by the projectiles.
Abstract:
A kinetic energy rod warhead with aligned projectiles includes a projectile core in a hull including a plurality of individual projectiles and an explosive charge in the hull about the core. The individual projectiles are aligned when the explosive charge deploys the projectiles. The projectiles may also be aimed in a specific direction.
Abstract:
A system and method for defending a vehicle against an approaching threat, is disclosed. A threat approaching the vehicle is identified. A rigid body is then deployed from the vehicle. Means associated with the body are provided for allowing controlled, guided propulsion of the body to position a reference axis of the body to a desired orientation relative to the threat and to translate the body substantially perpendicular to the reference axis, so as to eliminate the threat.
Abstract:
A system for defending a planet having a satellite against impact from an incoming body includes an explosive system and a propulsion system. The explosive system is adapted for deployment on the satellite and detonation thereon with sufficient explosive force to produce at least one ejectum to which is imparted a velocity increment sufficient for the ejectum to exceed the satellite's escape velocity and enter orbit about the planet. The propulsion system is adapted to be secured to at least one ejectum and impart a velocity increment to the ejectum sufficient to leave orbit about the planet and enter an orbit intercepting the incoming body.The system is used in a planetary defense method in which the explosive system is deployed at a deployment site on the satellite and detonated to produce at least one ejectum having a velocity that exceeds the escape velocity of the satellite. The ejectum enters into orbit around the planet, at which time the propulsion system is secured to the ejectum to produce a projectile. The propulsion system is then activated to increase the velocity of the projectile, causing the projectile to enter into an intercept orbit targeting the incoming body and subsequently intercept and impact the incoming body. The impact prevents the incoming body from impacting the planet.
Abstract:
A kinetic energy rod warhead with aligned projectiles includes a projectile core in a hull including a plurality of individual projectiles and an explosive charge in the hull about the core. The individual projectiles are aligned when the explosive charge deploys the projectiles. The projectiles may also be aimed in a specific direction.
Abstract:
A kinetic energy rod warhead with aligned projectiles includes a projectile core in a hull including a plurality of individual projectiles and an explosive charge in the hull about the core. The individual projectiles are aligned when the explosive charge deploys the projectiles. The projectiles may also be aimed in a specific direction.
Abstract:
A kinetic energy rod warhead deployment system and method featuring jettison housings each including a plurality of lengthy individual projectiles therein and a navigatable carrier for the jettison housings. The jettison housings are ejected in the vicinity of targets whereupon the individual projectiles are deployed in the trajectory path of each target.
Abstract:
A multipoint initiation system for an explosive including a stripline head and a plurality of detonators fixed to the head at predetermined locations. The head and detonators are embedded in the explosive without a mechanical safe-arm device. Electrical connections in the head provide for independent detonation of the detonators.