Aft-end ignition system for rocket motor

F - Mech Eng,Light,Heat,Weapons – 42 – C

Patent

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102/30

F42C 19/12 (2006.01) C06C 9/00 (2006.01) F02K 9/95 (2006.01) F42B 3/11 (2006.01) F42C 19/08 (2006.01)

Patent

CA 1036419

ABSTRACT An igniter for a rocket motor consisting of a cylindrical. tube having an open end and a closed end, a reduced section at the closed end, a plurality of segments extending outwardly from near the closed end, a squib secured in the reduced section, a charge in the tube and a polyurethane foam plug in the open end of the tube.

234045

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