Solid propellant canister loaded multiple pulsed or staged rocke

Power plants – Reaction motor – Motive fluid from diverse generators alternatively ejected...

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60250, 60253, F02K 928, F02K 934

Patent

active

049569716

ABSTRACT:
A multi-pulse or multi-stage canister loaded solid propellant rocket motor. The canisters are prepared separately and loaded with solid propellant whereby the scrap rate may be reduced after which they are installed in a monolithic case which affords stiffness continuity over the length of the rocket motor to prevent guidance system upsetting free play. In order to reduce the complexity of installation of the membrane seal assembly for each pulse, the bulkhead therefor is manufactured integral with the case of the respective canister and becomes the forward closure thereof. For the multi-stage rocket motor, the monolithic case may be stepped and tapered, and the stages severable therefrom as they burn out by primer cord.

REFERENCES:
patent: 3044255 (1962-07-01), Precoul
patent: 3173249 (1965-03-01), Wiggins
patent: 3442084 (1969-05-01), Dilchert et al.
patent: 3568448 (1971-03-01), Webb, Jr.
patent: 3812671 (1974-05-01), Burr et al.
patent: 3888079 (1975-06-01), Diesinger
patent: 4104878 (1978-08-01), Chase
patent: 4766726 (1988-08-01), Tackett et al.

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