IWIS 2021 - ID168 - Missile Engine Exhaust Nozzle

International Warsaw Invention Show IWIS 2021 Invention ID168 Title: Missile Engine Exhaust Nozzle Short description: The invention relates to a missile control system using hybrid thrust vector control. The solution combines a pivoting nozzle and cooperating movable jet vanes. The purpose of the invention is to increase the maneuverability of the missile during each phase of flight, resulting in increased defensive capabilities and guidance accuracy. Kielce University of Technology, Faculty of Mechatronics and Mechanical Engineering, #/en/Invention/168/