Desensitized solid rocket propellant formulation

Explosive and thermic compositions or charges – Containing inorganic oxygen-halogen salt – Alkali metal oxygen-halogen salt

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149 76, C06B 2922

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active

054746256

ABSTRACT:
A composite propellant composition and process are disclosed for reducing e reactive violence during cook-off and to improve the performance of a potassium perchlorate/ammonium perchlorate propellant composition wherein 0.25-2.0% by weight, of iron oxide replaces 0.25-2.0% by weight, of potassium perchlorate in the composition.

REFERENCES:
patent: 3986908 (1976-10-01), Grebert et al.
patent: 4246051 (1981-01-01), Garner et al.
patent: 4776993 (1988-10-01), Chang
patent: 4881994 (1989-11-01), Rudy et al.

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