Chlorine-free solid rocket propellant for space boosters

Explosive and thermic compositions or charges – Structure or arrangement of component or product – Solid particles dispersed in solid solution or matrix

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149 194, 149 196, 149 20, 149 22, C06B 4510

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active

052717780

ABSTRACT:
A stable chlorine-free solid rocket propellant composition containing a low energy binder component having an HEX value not exceeding about 0 cal/gm and comprising, in combination, a nitrate salt and/or phase stabilized nitrate salt as oxidizer component, a Mg/Al alloy of limited Mg content as a fuel component, at least one energetic plasticizer component, and a burn rate catalyst.

REFERENCES:
patent: 3350245 (1967-10-01), Dickinson
patent: 3445304 (1969-05-01), Cahill et al.
patent: 3873386 (1975-03-01), Elrick
patent: 4158583 (1979-06-01), Frosch
patent: 4165247 (1979-08-01), Brew et al.
patent: 4318270 (1982-03-01), Orlick et al.
patent: 4642147 (1987-02-01), Hyyppa
patent: 4919737 (1990-04-01), Biddle et al.
patent: 4925909 (1990-05-01), Kubota et al.
patent: 4976794 (1990-12-01), Biddle et al.
patent: 5074938 (1991-12-01), Chi
patent: 5076868 (1991-12-01), Doll et al.

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