Fail safe rocket motor

Power plants – Reaction motor – Solid propellant

Patent

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60 3947, F02K 900

Patent

active

044943733

ABSTRACT:
In a rocket motor having an insulative coating on selected portions of the xterior casing, one or more ribs are used to structurally strengthen portions of the casing and to reinforce thermal stress patterns which will cause failure venting at a predetermined point of the rocket motor as a cook-off safety feature.

REFERENCES:
patent: 2175071 (1939-10-01), Walker
patent: 2787397 (1957-04-01), Radford
patent: 3175497 (1965-03-01), Head
patent: 3265310 (1966-08-01), Cohen
patent: 3440820 (1969-04-01), Caveny
patent: 3499283 (1970-03-01), Simpkins
patent: 3664133 (1972-05-01), Iwanciow et al.
patent: 3713395 (1973-01-01), Carpenter et al.
patent: 3970208 (1976-07-01), Raes

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