High burning rate propellants with coprecipitated salts of decah

Details High burning rate propellants with coprecipitated salts of decah High burning rate propellants with coprecipitated salts of decah

1976-07-22

1979-02-06

Miller, Edward A.

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

149 191, 149 193, 149 199, 149 22, C01B 4510

Patent

active

041382820

ABSTRACT:
A class of high burning propellants, useful as gun or rocket propellants, gas generators or specialized application where a very high burning rate is required, characterized by replacing the normally found oxidizer used in various propellants with certain coprecipitated salts of decahydrodecaboric acid and certain oxidizing agents. The resultant propellants employ such a coprecipitate as the major faction of the solids loading, and optionally may further include certain simple decahydrodecaborate salts for further enhancement of the burning rates in the thusly formulated and composed propellants.

REFERENCES:
patent: 3126305 (1964-03-01), Armstrong
patent: 3148938 (1964-09-01), Knoth
patent: 3149163 (1964-09-01), Knoth
patent: 3256056 (1966-06-01), Armstrong
patent: 3617403 (1971-11-01), Johnson
patent: 3689331 (1972-09-01), Pierce
patent: 4002681 (1977-01-01), Goddard

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