Supersonic missile flight control system - has air intakes in shell between tip and body connected to control nozzles in shell wall via reservoir and fluid elements

摘要

The flight correction device for a supersonic missile (1) with an air breathing thrust control system includes at least three air intakes (5) in the shell at the transition between the missile tip (3) and body (2) and leading to a reservoir (7). The device also has two or more fluid elements (8-11) aligned behind each other along the missile axis (100) and connected to the reservoir (7) via orifices (12-15). Control nozzles (6) are spaced around the missile body (2) in each fluid element (8-11). USE/ADVANTAGE - For correcting flight of supersonic missile. Does not use expensive swivelling side inlets and has high firing strength.