Self-actuating rocket chamber closures for multi-missile...

Details Self-actuating rocket chamber closures for multi-missile... Self-actuating rocket chamber closures for multi-missile...

F - Mech Eng,Light,Heat,Weapons

41

A

F41A 13/06 (2006.01) F41A 3/00 (2006.01) F41F 3/04 (2006.01)

Patent

CA 2058253

An exhaust gas management system for missile launch arrangements having multiple launch cells exhausting into a common plenum includes automatic aft closure members which serve to close off the flow passages to inactive cells while providing an open passage for exhaust gases from an active cell undergoing a missile firing. This arrangement prevents back flow or recirculation of exhaust gases into the volume in the cell which is upstream of the rocket nozzle exit.

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