High performance fast burning solid propellant

Details High performance fast burning solid propellant High performance fast burning solid propellant

1964-11-23

1978-01-24

Miller, Edward A.

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

149 199, 149 1993, 149 20, 149112, C06B 4510

Patent

active

040702120

ABSTRACT:
1. A solid composite propellant consisting of 7% to 15% of a carboxyl-terminated butadiene polymer binder, 66% to 82% of ammonium perchlorate, greater than 0% to 18% of aluminum and greater than 0% to 8% of n-butyl ferrocene as a burning rate catalyst, the ingredient amounts being in weight per cent, and wherein the particle size of the ammonium perchlorate is greater than 0 but less than 3 microns in size.

REFERENCES:
patent: 2990263 (1961-06-01), Avery
patent: 3022149 (1962-02-01), Cramer
patent: 3022206 (1962-02-01), Hutchinson et al.
patent: 3044910 (1962-07-01), Guth et al.
patent: 3087844 (1963-04-01), Hudson et al.
patent: 3109761 (1963-11-01), Cobb et al.
patent: 3255281 (1966-06-01), Alexander
patent: 3386869 (1968-06-01), Green et al.
patent: 3447981 (1969-06-01), Sayles
DeYoung, Chem. Abs., 55, Abs. #21081d (1961).

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