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U.S. Department of Energy
Office of Scientific and Technical Information

A processing method for increasing propellant burning rate

Patent ·
OSTI ID:6799600
A processing method is described comprising milling in a roller mill; a propellant composition paste comprised of about 9.7 weight percent of a hydroxyl-terminated polybutadiene prepolymer binder system with an antioxidant content of about 0.1% to about 0.6% of polybutadiene polymer, and of an isophorone diisocyanate curing agent content of about 0.5% to about 2.0% of polybutadiene polymer; isophthaloyl bis-1-(2-methylaziridine) of about 0.3 weight percent; dioctyl adipate of about 2.0 weight percent; fluid-energy mill-ground ammonium perchlorate of about 86.0 weight percent; aluminum powder of about 1.0 weight percent; and iron oxide of about 1.0 weight percent. The burning rate and mechanical properties of the propellant composition are improved as compared with using a sigma blade mixer to mix a like propellant composition paste, the improvement in burning rate being increased from about 1.6 inches per second to about 2.8 inches per second at about 2000 psi. The mechanical property of stress is increased from about 145 to about 245 psi, the mechanical property of strain at maximum stress being increased from about 40 to about 45%, and the mechanical property of modulus being increased from about 290 to about 950 psi.
Assignee:
The Secretary of the Army, Washington, DC
Patent Number(s):
US 4655860
OSTI ID:
6799600
Country of Publication:
United States
Language:
English