Slot former assembly for use in solid propellant rocket motors

Ammunition and explosive-charge making – Miscellaneous

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264 3R, C06B 2100

Patent

active

039526275

ABSTRACT:
1. A slot former assembly for use in fabricating the solid propellant in a motor case for a solid propellant rocket motor comprising an outer hollow core, an inner tubular core and a flexible slot former comprising a skeleton frame consisting of stiffening rods that are retained in spaced relation to each other by means of a cord woven thereon in a basket weave and provided with a covering of flexible material operatively connected to said hollow core, whereby when said assembly is positioned in said motor case and the solid propellant is cast therein about said assembly, a slotted cavity configuration will be provided in the solid propellant in said motor case.

REFERENCES:
patent: 2164310 (1952-10-01), James
patent: 2847708 (1958-08-01), Hamjian
patent: 2920443 (1960-01-01), Higginson
patent: 2952876 (1960-09-01), Miles
patent: 3009385 (1961-11-01), Burnside
patent: 3052945 (1962-09-01), Cummings
patent: 3064423 (1962-11-01), Frey
patent: 3120028 (1964-02-01), Streeter et al.
patent: 3136831 (1964-06-01), Zinn

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