Pressure relief device for solid propellant motors subjected to

Details Pressure relief device for solid propellant motors subjected to Pressure relief device for solid propellant motors subjected to

1990-03-05

1991-08-06

Casaregola, Louis J.

Power plants

Reaction motor

Solid propellant

60 391, F02K 100

Patent

active

050366580

ABSTRACT:
A rocket motor that has a solid propellant with closure means that is secd to the rocket motor housing by heat responsive means that melts before the solid propellant ignites to prevent the rocket motor from becoming propulsive when subjected to excessive external heat sufficient to cause the rocket propellant to ignite.

REFERENCES:
patent: 2958184 (1960-11-01), Sanders
patent: 2958185 (1960-11-01), Sanders
patent: 3134222 (1964-05-01), Maxon
patent: 3613374 (1971-10-01), Ritchey
patent: 3887991 (1975-06-01), Panella
patent: 4423683 (1984-01-01), Telmo

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