May 19, 2026
A hybrid pad system positioned between a missile and a launch tube is provided herein. The hybrid pad system includes an outer sheet and an inner sheet spaced from the outer sheet. A web region can be positioned between the outer sheet and the inner sheet. A restoration region can be positioned between the outer sheet and the inner sheet and tangentially offset from the web region. A support can be operably coupled with the inner sheet.
May 12, 2026
A Single Armament Control Unit (SACU) that operates a single missile tube as opposed to multiple tubes. The SACU provides for interlock pin and umbilical depression from the housing on the rotation of a single crankshaft controlled by a single motor where the rotor of the motor and the rotational axis of the crankshaft are generally parallel to the missile tube.
May 5, 2026
An aircraft comprising a weapons pod including an enclosure mounted to an outer mold line of the aircraft, and at least one missile rail launcher mounted entirely within and fixed to the enclosure.
Apr 28, 2026
A mounting system and method that provides simplified mounting points and attachment interfaces for associated components. Specifically, the system and method generally comprise a mounting system, including a new support chassis, which allows for a Forward Looking Infrared (FLIR) aiming system which was built to be placed in an infantry system for a TOW missile, to be used in a vehicle mounted ISU system.
Jul 8, 2025
A missile for delivering a payload and having a longitudinal axis. The missile comprises a nonfragmenation multi-directional munition having a hollow collar. The hollow collar has an inner surface and an outer surface opposed thereto and a first plurality of ports extending therebetween in a substantially radial direction. An ammunition is disposed in each port of the first plurality of ports, oriented outwardly from the longitudinal axis with an ignition source for expelling such ammunition from the collar. The missile also has at least one flight control surface for controlling a trajectory of the missile during flight and a controller for controlling the flight of the missile and the ignition source.
