Ram air steering system for a guided missile

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

F - Mech Eng,Light,Heat,Weapons

02

K

60/67

F02K 9/00 (2006.01) F42B 10/66 (2006.01)

Patent

CA 1204600

Abstract An opening in the nose of a missile allows entry of ram air during missile flight to a central chamber. Oppositely oriented steering jets are interconnected with the aft end of the central chamber and escaping ram air provides lateral steering thrust forces. A movable diverting means controls the direction that the escaping ram air is diverted and therby controls the steering forces.

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