A projectile launch detector, including a body, a mast and a blade rigidly connected to the mast; the mast being capable of sliding between a retracted configuration and a deployed configuration, and capable of pivoting between a first and a second angular position. The detector may further includes a first elastic return element to return the mast to the deployed configuration relative to the body; and a first associated sensor; and a second elastic return element to return the mast to the first angular position relative to the body; and a second associated sensor.

A projectile launch detector including a body, a mast and a blade rigidly connected to the mast; the mast being capable of sliding between a retracted configuration and a deployed configuration, and capable of pivoting between a first and a second angular position. The detector may further include a first elastic return element to return the mast to the deployed configuration relative to the body; and a first associated sensor; and a second elastic return element to return the mast to the first angular position relative to the body; and a second associated sensor.

A buoyant energy device is disclosed. Differing specific gravities between various materials are used to drive turbine blades to create energy by cycling the materials through a turbine activation area. The materials include water, oils, gasses (lighter than air and ambient air), or various other materials as circumstances may require. The device produces electricity that may be stored or used immediately. It is contemplated that the device could be used to power a missile, a torpedo, static mines, or the like.

An extended range support module for an undersea vehicle includes an outer hull capable of accommodating the undersea vehicle therein. A navigation module is positioned on the outer hull and capable of being joined to the undersea vehicle. Controllable fins are provided on the outer hull and joined to allow control by the navigation module. A buoyancy control system is positioned within the outer hull and joined to the navigation module. An extended fuel tank is provided inside the outer hull between the outer hull and the undersea vehicle. The extended fuel tank is joined to provide fuel to the undersea vehicle. The navigation module can have GPS, inertial sensors, and sonar sensors to aid in navigation.

An extended range support module for an undersea vehicle includes an outer hull capable of accommodating the undersea vehicle therein. A navigation module is positioned on the outer hull and capable of being joined to the undersea vehicle. Controllable fins are provided on the outer hull and joined to allow control by the navigation module. A buoyancy control system is positioned within the outer hull and joined to the navigation module. An extended fuel tank is provided inside the outer hull between the outer hull and the undersea vehicle. The extended fuel tank is joined to provide fuel to the undersea vehicle. The navigation module can have GPS, inertial sensors, and sonar sensors to aid in navigation.

An aircraft, missile, projectile, or underwater vehicle with an improved control system, an improved control system, or a method of maneuvering an aircraft, missile, projectile, or underwater vehicle uses control surfaces that are movable along a track. The control system on a track (or tracked control surface) advantageously enables the aircraft, missile, projectile, or underwater vehicle to have an unlimited number of configurations, each configuration being tailored to the specific stability or maneuverability requirements during a specific portion of the flight by adjusting the center of pressure of the aircraft, missile, projectile, or underwater vehicle relative to its center of gravity.

An aircraft, missile, projectile, or underwater vehicle with an improved control system, an improved control system, or a method of maneuvering an aircraft, missile, projectile, or underwater vehicle uses control surfaces that are movable along a track. The control system on a track (or tracked control surface) advantageously enables the aircraft, missile, projectile, or underwater vehicle to have an unlimited number of configurations, each configuration being tailored to the specific stability or maneuverability requirements during a specific portion of the flight by adjusting the center of pressure of the aircraft, missile, projectile, or underwater vehicle relative to its center of gravity.