Claims
- 1. A method of achieving an ultrahigh-burning rate for a composite solid propellant composition comprised of a hydroxyl-terminated polybutadiene binder system including an polyisocyanate curative as an additive of up to about 1 weight percent, an ammonium perchlorate oxidizer, and an aluminum metal fuel, said method comprising:
- (i) providing said composite solid propellant composition in an uncured homogeneously mixed state which comprises a weight percent range from about 95 to about 99 of said ultrahigh burning rate composite solid propellant composition;
- (ii) providing a solid explosive composition of diazodinitrophenol of predetermined shapes and dimensions of cubes or pellets, said dimension when of a cube shape being from about 1/16 inch to about 3/32 inch on each side, and said dimension when of a pellet shape being from about 1/16 inch to about 3/32 inch diameter;
- (iii) adding a predetermined amount from about 1 weight percent to about 5 weight percent of said diazodinitrophenol to said weight percent ranges of said uncured homogeneously mixed composite solid propellant composition;
- (iv) mixing said uncured uniformly mixed composite solid propellant composition with said added amount of said diazodinitrophenol to achieve a homogenous mixture; and,
- (v) curing said uncured uniformly mixed composite solid propellant containing said diazodinitrophenol to yield an ultrahigh-burning rate composite solid propellant grain wherein said diazodinitrophenol functions as a burn rate accelerator.
- 2. The method of achieving ultrahigh-burning rate for a composite solid propellant composition as defined in claim 1 where in said diazodinitrophenol is 2-diazo-4,6-dinitrophenol and wherein said hydroxyl-terminated polybutadiene binder system is present in an amount from 9 to about 12 weight percent, said ammonium perchlorate oxidizer is present in an amount from about 65 to about 78 weight percent, and said aluminum metal fuel is present is an amount from about 20 weight percent.
- 3. The method of achieving ultrahigh burning rate for a composite solid propellant composition as defined in claim 2 wherein said 2-diazo-4,6-dinitrophenol is employed in said predetermined shape of pellets with dimension of 1/16 inch diameter and in said predetermined amount of about 4.5 weight percent to produce a burning rate increase from about 0.6 inches per second at 0 weight percent of said 2-diazo-4,6-dinitrophenol to about 4.5 inches per second with said weight percent of said 2-diazo-4,6-dinitrophenol.
- 4. The method of achieving ultrahigh-burning rate for a composite solid propellant composition as defined in claim 2 wherein said 2-diazo-4,6-dinitrophenol is employed in said predetermined shape of cubic pellets with dimension of 3/32 inch on each side and in said predetermined amount of about 4.5 weight percent to produce a burning rate increase from about 0.6 inches per second at 0 weight percent of said 2-diazo-4,6-dinitrophenol to about 6.5 inches per second with said weight percent of said 2-diazo-4,6-dinitrophenol.
Government Interests
The invention described herein may be manufactured, used, and licensed by or for the Government for governmental purposes without the payment to me of any royalties thereon.
US Referenced Citations (6)