Composite propellants containing critical pressure increasing ad

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 18, 149 191, 149 1992, 149 20, C06B 4510

Patent

active

039869105

ABSTRACT:
Increasing the critical pressure of composite propellants by admixing into he propellant composition an additive selected from the group consisting of (1) oxides of Group II metals, titanium, aluminum, boron, zirconium, and lead; (2) nitrides of Group II metals, aluminum, and boron; (3) carboxylates, formates, and sulfates of Group II metals, aluminum, calcium, and magnesium; (4) hydrates of the carboxylates, formates, and sulfates of Group II metals, aluminum, calcium, and magnesium; (5) the following fibrous materials, asbestos, quartz, carbon, and boron; (6) the following metal: Group II metals and boron; and (7) mixtures thereof.

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patent: 3359350 (1967-12-01), Godfrey
patent: 3392068 (1968-07-01), Knowles et al.
patent: 3476622 (1969-11-01), Harada et al.
patent: 3520742 (1970-07-01), Witz
patent: 3577289 (1971-05-01), Morrell
patent: 3682727 (1972-08-01), Heinzelmann et al.
patent: 3822154 (1974-07-01), Lawrence et al.

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