Propellants

F - Mech Eng,Light,Heat,Weapons – 02 – K

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52/49, 60/71

F02K 9/10 (2006.01) F02K 9/34 (2006.01)

Patent

CA 1171292

JX/3428/04 A B S T R A C T Canada The emission of smoke from rocket motors, especially those using "smokeless" double-base propellant systems may be reduced by using as the inhibiting coating on the propellant and/or as thermal insulation an elastomeric composition comprising a silicone rubber filed with asbestos. The asbestos should preferably be fibrous with an aspect ratio above about 10 : 1 and should comprise at least 10% w/w of the elastomeric composition. Preferred silicone rubber are room-temperature curing organopolysiloxane/ alkyl silicate systems.

163326

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