A composite propellant composition and process are disclosed for reducing the 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.
Desensitized Solid Rocket Propellant Formulation
1993
9 pages
Report
Keine Angabe
Englisch
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