Lateral thrust assembly for missiles

Details Lateral thrust assembly for missiles Lateral thrust assembly for missiles

F - Mech Eng,Light,Heat,Weapons

42

B

F42B 10/66 (2006.01) B64C 15/14 (2006.01) B64G 1/00 (2006.01) F02K 9/80 (2006.01) F02K 9/88 (2006.01) F41G 7/00 (2006.01) F42B 10/00 (2006.01)

Patent

CA 2064208

2064208 9101478 PCTABS00003 A lateral thrust assembly (12) for missile maneuvering comprises an annular array of outwardly directed nozzles (22) each nozzle having a releasable plug (26) normally blocking flow of propellant gases out of the nozzle. A plug release mechanism (38) associated with each plug allows that plug to be released to open the respective nozzle. A combustion chamber (32) containing propellant is connected to the inner ends of all the nozzles. The propellant is ignited when one or more selected plugs are released to allow opening of the associated nozzle or nozzles, controlling the direction of the lateral thrust applied to the vehicle.

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