Solid rocket propellants comprising guignet's green pigment

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, 149 199, 149 20, 149 76, 149 86, C06B 4506

Patent

active

044117175

ABSTRACT:
A solid rocket propellant composition comprising a major amount of ammonium perchlorate, a minor amount of aluminum powder, a minor amount of a binder, and an effective, burn rate modifying amount of Guignet's green pigment or oxidized Guignet's green. Guignet's green pigment increases the burn rate of the propellant without unacceptably increasing the pressure dependence of the burn rate.

REFERENCES:
patent: 2740702 (1956-04-01), Mace
patent: 3151010 (1964-09-01), Bize
patent: 3259531 (1966-07-01), Lofberg
patent: 3664898 (1972-05-01), Taylor et al.
patent: 3748199 (1973-07-01), Vriesen et al.
patent: 3830675 (1974-08-01), Zelinski et al.
patent: 3948698 (1976-04-01), Elrick et al.

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