Abstract: Provided is a modular directional charge system that can be assembled in different configurations depending on the target. The system includes a removable energetic material, a molded plastic shell comprising a main body and a front cover, a removable fragmentation insert, a removable breaching insert, an initiator well insert, and initiator adapter nuts. The main body comprises an internal energetic material receiving compartment, a first and second tripod mount, a threaded adapter, and a pair of pin receivers, while the front cover comprises an internal removable insert compartment. The main body and front cover are held together with a multi-position adjustable toothed locking interface that adjustably permits the cover to intimately contact the energetic material when the internal removable insert compartment contains a fragmentation insert, a breaching insert, or no insert at all. A method of use is also provided.

Abstract: Various embodiments of optimized subsonic projectiles are provided. For example, one exemplary subsonic projectile can include an elliptical nose cone, a cylindrical body and a boattail with various design features that can be used in a subsonic ammunition cartridge where the subsonic projectile is stabile throughout at least a segment of a flight allowing for better accuracy, maintaining low drag, maximizing range and achieving desired performance while ensuring the projectile stays below the speed of sound and lowering a noise profile of projectile and a launcher firing the projectile.

Abstract: Provided is a modular directional charge system that can be assembled in different configurations depending on the target. The system includes a removable energetic material, a molded plastic shell comprising a main body and a front cover, a removable fragmentation insert, a removable breaching insert, an initiator well insert, and initiator adapter nuts. The main body comprises an internal energetic material receiving compartment, a first and second tripod mount, a threaded adapter, and a pair of pin receivers, while the front cover comprises an internal removable insert compartment. The main body and front cover are held together with a multi-position adjustable toothed locking interface that adjustably permits the cover to intimately contact the energetic material when the internal removable insert compartment contains a fragmentation insert, a breaching insert, or no insert at all. A method of use is also provided.

Abstract: Various embodiments of optimized subsonic projectiles are provided. For example, one exemplary subsonic projectile can include an elliptical nose cone, a cylindrical body and a boattail with various design features that can be used in a subsonic ammunition cartridge where the subsonic projectile is stabile throughout at least a segment of a flight allowing for better accuracy, maintaining low drag, maximizing range and achieving desired performance while ensuring the projectile stays below the speed of sound and lowering a noise profile of projectile and a launcher firing the projectile.

Abstract: Various embodiments of optimized subsonic projectiles are provided along with related methods. For example, one exemplary subsonic projectile can include an elliptical nose cone, a cylindrical body and a boattail with various design features that can be used in a subsonic ammunition cartridge where the subsonic projectile is stabile throughout at least a segment of a flight allowing for better accuracy, maintaining low drag, maximizing range and achieving desired performance while ensuring the projectile stays below the speed of sound and lowering a noise profile of projectile and a launcher firing the projectile.

Abstract: Various embodiments of optimized subsonic projectiles are provided along with related methods. For example, one exemplary subsonic projectile can include an elliptical nose cone, a cylindrical body and a boattail with various design features that can be used in a subsonic ammunition cartridge where the subsonic projectile is stabile throughout at least a segment of a flight allowing for better accuracy, maintaining low drag, maximizing range and achieving desired performance while ensuring the projectile stays below the speed of sound and lowering a noise profile of projectile and a launcher firing the projectile.

Abstract: An adapter for mounting on a weapon. The adapter illustratively includes a plurality of mounting rails for removably coupling with a variety of accessories, such as sights, illumination devices, and laser aiming devices.

Abstract: An adapter for mounting on a weapon. The adapter illustratively includes a plurality of mounting rails for removably coupling with a variety of accessories, such as sights, illumination devices, and laser aiming devices.

Abstract: A weather monitoring and prediction system that uses a fleet of aircraft to obtain data. Each aircraft has a local air data system that facilitates the measurement, recordation, and transmittal of local atmospheric data such as barometric pressure, and the corresponding temporal, positional, and altitudinal data. The data is electronically transmitted from each aircraft to a ground based processing system where it is stored. The data may then be transmitted to subscribing users such as aircraft, other weather data systems or to air traffic control centers in either a compiled form or in a raw form. Another embodiment also provides for measuring barometric pressure as a function of altitude at an in-flight aircraft.

Abstract: A weather monitoring and prediction system that uses a fleet of aircraft to obtain data. Each aircraft has a local air data system that facilitates the measurement, recordation, and transmittal of local atmospheric data such as barometric pressure, and the corresponding temporal, positional, and altitudinal data. The data is electronically transmitted from each aircraft to a ground based processing system where it is stored. The data may then be transmitted to subscribing users such as aircraft, other weather data systems or to air traffic control centers in either a compiled form or in a raw form. Another embodiment also provides for measuring barometric pressure as a function of altitude at an in-flight aircraft.