Aft-end ignition system for rocket motor

Ammunition and explosives – Igniting devices and systems

Patent

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Details

60 3982E, 60256, F42C 1912

Patent

active

040234975

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.

REFERENCES:
patent: 2776623 (1957-01-01), Bonner
patent: 2990683 (1961-07-01), Walden
patent: 3251267 (1966-05-01), Hauser et al.
patent: 3746214 (1973-07-01), Stephenson
patent: 3974772 (1976-08-01), Pelham

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