Composite propellant compositions

Details Composite propellant compositions Composite propellant compositions

C - Chemistry, Metallurgy

06

B

C06B 23/00 (2006.01) C06B 45/10 (2006.01) C06D 5/06 (2006.01)

Patent

CA 2506257

The invention relates to propellant compositions comprising a solid inorganic perchlorate oxidizing agent, a nitrogen-containing fuel, and a burn rate catalyst. Such compositions may be used as a propellant material, (e.g., in rocketry), a pyrotechnie material, an explosive material, a light generating material, a heat generating material, or a sound generating material.

L'invention concerne des compositions d'agent propulsif hétérogène comprenant un agent oxydant à base de perchlorate inorganique, un combustible azoté, et un catalyseur augmentant la vitesse de combustion. Ces compositions peuvent servir de matériau de propulsion (p. ex. dans le domaine de la fuséonautique), de matériau pyrotechnique, de matériau explosif, de matériau générateur de lumière, de matériau thermogène, ou de matériau générateur de son.

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