F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
60/71
F02K 9/70 (2006.01) F02K 9/26 (2006.01) F02K 9/34 (2006.01) F02K 9/36 (2006.01)
Patent
CA 1166854
ABSTRACT OF THE INVENTION: A solid propellant rocket motor or gas generator of the type having retractable filaments embedded in the propellant for the purpose of controlling the overall thrust or mass flow output is combined with a channeled separator located between the propellant and its casing with the channels open to the combustion chamber. This results in distribution of combustion chamber pressure and temperatures over the exterior of the propellant grain so that distortion of the grain will not occur sufficiently to cause binding or sticking of the filament in their holes in the propellant nor will the holes be enlarged to cause uncontrolled burning between the filament and the hole.
361321
Cordant Technologies Inc.
Gowling Lafleur Henderson Llp
LandOfFree
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