Integrated propulsion and attitude control system from a common pressure vessel for an interceptor

This invention describes a compact, lightweight missile designed to intercept targets. It uses a single rocket motor where the burning fuel creates high-pressure gas, which is then split to provide both forward propulsion and steering. Some gas exits through fixed nozzles at the rear for thrust, while other gas is directed through small side nozzles at the front to control the missile's direction. This specific design is for very small interceptors, weighing under 6.8 kilograms, and aims to keep the steering energy minimal.