Abstract: A deployable shroud provides an aerodynamically smooth surface to minimize the drag otherwise experienced by blunt nose projectiles. The shroud comprises multiple petals mounted at the nose of the projectile that are released at a set time during flight. The deployment mechanism assembly of the shroud provides deployment of the petals without the generation of shock waves into the projectile and comprises a fusible link powered by a thermal source. The shroud assembly is self-powered and does not require energy input from the projectile.

Abstract: A ground surface reconnaissance projectile includes a tube-launched 60 mm inert mortar round, which remotely relays reconnaissance and surveillance data back to an operator, after it has landed and uprighted itself. The types of collected data include for example, visual imagery of the target area in 360 degrees, acoustic target tracking and voice recognition, infra-red motion detection, and magnetic field disturbance sensing.

Abstract: A round for launching from a gun may include a cartridge case and a projectile body adjacent the cartridge case. A pusher may be disposed in the cartridge case and may be operable to push the projectile body upon firing the round. An imaging sensor may be disposed at least partially in the projectile body. The imaging sensor may include a sensor base and a sensor lens. A first kinetic energy absorber may be disposed around the sensor base. A second kinetic energy absorber may be disposed around the sensor lens. After the round is fired and the pusher exits the gun, the pusher may separate from the projectile body and the second kinetic energy absorber may separate from the imaging sensor.