Solid propellant rocket motor with fusible end closure holder

Power plants – Combustion products used as motive fluid – Different fluids

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102481, 220 894, F02K 100

Patent

active

H00011444

ABSTRACT:
A solid propellant rocket motor comprising a motor case, solid propellant and at least one end closure, wherein at least one end closure is connected to the casing by at least one fusible connector which melts at temperatures below those that will cause autoignition of the motor but does not melt during normal propulsion, so that the end closure releases before the antoignition and is retained in place during normal propulsion.

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patent: 5036658 (1991-08-01), Tate

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