Embedded explosives as burning rate accelerators for solid prope

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 42, 149 76, 149 88, C06B 4510

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active

050153102

ABSTRACT:
A method of achieving an ultrahigh-burning rate composite solid propellant hrough the embedment of the solid explosive diazodinitrophenol (e.g., 2-diazo-4,6-dinitrophenol) having predetermined shapes and dimensions of cubes or pellets. Cubes having dimension from about 1/16 inch to about 3/32 inches on each side and pellets having dimensions from about 1/16 inch to about 3/32 inch diameters are employed in weight percent ranging from about 1 to about 5 with an uncured composite solid propellant composition in a weight percent range from about 95 to about 99. After being uniformly blended in the uncured state, the propellant and solid explosive are cured to a solid grain which has an increase in burning rate with about a 4.5 weight percent concentration of diazodinitrophenol of about 4.5 composite solid propellant composition with 0% diazodinitrophenol burned at 0.6 inches per second. A typical composite solid propellant composition has a range of hydroxy-terminated polybutadiene binder with an added polyisocyanate curative of about 1 weight percent from about 9 to about 12 weight percent, a range of ammonium perchlorate oxidizer from about 65 to about 78 weight percent, and a range of aluminum metal fuel from about 10 to about 20 weight percent.

REFERENCES:
patent: 3798090 (1974-03-01), Anabashi
patent: 4092189 (1978-05-01), Betts
patent: 4441942 (1984-04-01), Sayles
patent: 4530728 (1985-07-01), Sayles
patent: 4655858 (1987-04-01), Sayles
patent: 4952254 (1990-08-01), Betts et al.

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