Stress relief system for slotted propellant motors

Ammunition and explosives – Powder form – Having embedded reinforcing or burning control means

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Details

102288, C06B 4500

Patent

active

053850998

ABSTRACT:
The present invention is for a means to relieve stress in slotted solid propellant rocket motors. The invention provides for one or more articulated members located between the outer edge of a secondary slot and the layer of thermal insulation. Also disclosed is a method of forming the articulated members.

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