Ram air combustion steering system for a guided missile

Details Ram air combustion steering system for a guided missile Ram air combustion steering system for a guided missile

F - Mech Eng,Light,Heat,Weapons

02

K

60/67

F02K 9/00 (2006.01) F02K 7/18 (2006.01) F02K 9/80 (2006.01) F41G 7/00 (2006.01) H04K 1/02 (2006.01)

Patent

CA 1207154

ABSTRACT An open-ended diffusion chamber and an adjacent combustion chamber located in the nose of a projectile to receive ram air that ignites a solid fuel material within the combustion chamber. A pair of oppositely disposed lateral steering ports are provided aft of the combustion chamber and are interconnected therewith via a diverting valve that is controllable to selectively divert the escaping combustion gases from the combustion chamber to one or both of the steering ports to thereby change or maintain the trajectory course of the projectile after firing.

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