Solid propellant with alumina burning rate catalyst

Details Solid propellant with alumina burning rate catalyst Solid propellant with alumina burning rate catalyst

1976-04-22

1978-04-18

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 18, 149 191, 149 199, 149 21, 149110, C06B 4508

Patent

active

040849929

ABSTRACT:
Finely divided aluminum oxide increases the burning rate, reduces the pressure exponent at high pressures and stabilizes the combustion of solid propellant compositions.

REFERENCES:
patent: 3310946 (1967-03-01), Dobbins
patent: 3822154 (1974-07-01), Lawrence et al.
patent: 3924405 (1975-12-01), Cohen et al.
patent: 3986906 (1976-10-01), Sayles

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