Centerport inhibitor for a solid propellant rocket motor, a solid propellant rocket motor including same, and a method of inhibiting a centerport of a solid propellant rocket motor
A pourable opaque centerport for solid propellant rocket motors and method for applying the same are disclosed. The pourable centerport inhibitor for solid propellant rocket motors has a curing system that includes a prepolymer and a curing agent. The prepolymer and the curing agent are combined to form a pourable polymeric binder that cures into an amorphous solid. The pourable centerport inhibitor also includes an opaque agent. The pourable centerport inhibitor may also include a plasticizer. The plasticizer, the prepolymer, and the curing agent are preferably the same type that is in the solid propellant with which it will be used in conjunction.
1. A pourable centerport inhibitor for a solid propellant rocket motor, consisting essentially of:
a hydroxyl terminated polybutadiene; and
a multifunctional isocyanate, wherein the hydroxyl terminated polybutadiene and the multifunctional isocyanate are combined to form a pourable polymeric binder that cures into an amorphous solid.
2. The pourable centerport inhibitor of claim 1 , further comprising an opaque agent.
3. The pourable centerport inhibitor of claim 2 , further comprising a plasticizer.
4. The pourable centerport inhibitor of claim 3 , wherein the plasticizer, the hydroxyl terminated polybutadiene, and the multifunctional isocyanate are the same type used in a solid propellant.
5. A method of inhibiting a centerport of a solid propellant rocket motor, comprising:
pouring an amount of uncured inhibitor into a centerport of a solid propellant rocket motor, wherein the uncured inhibitor consists essentially of a hydroxyl terminated polybutadiene and a multifunctional isocyanate; and
rotating the solid propellant rocket motor in a substantially horizontal position for a period of time that allows the uncured inhibitor to cure.
6. The method of claim 5 , further comprising forming a chemical bond between the uncured inhibitor and a solid propellant as the uncured inhibitor cures.
7. The method of claim 5 , further comprising pouring an additional amount of the uncured inhibitor into the centerport of the solid propellant rocket motor and rotating the solid propellant rocket motor in the substantially horizontal position for a period of time that allows the additional amount of the uncured inhibitor to cure to increase a thickness of a centerport inhibitor.
8. A solid propellant rocket motor with an inhibited centerport, comprising:
a rocket motor case;
a solid propellant having a centerport; and
a centerport inhibitor that consists essentially of a hydroxyl terminated polybutadiene and a multifunctional isocyanate,
wherein the solid propellant is positioned inside the rocket motor case and wherein the centerport inhibitor is bonded to a surface of the centerport of the solid propellant in an even distribution.
9. The solid propellant rocket motor of claim 8 , wherein the solid propellant and the centerport inhibitor have compatible cure systems.
10. The solid propellant rocket motor of claim 8 , wherein the solid propellant and the centerport inhibitor utilize the same cure systems.
11. The solid propellant rocket motor of claim 8 , wherein the solid propellant and the centerport inhibitor utilize the same cure systems and same plasticizers.
12. The solid propellant rocket motor of claim 11 , wherein the plasticizer in the solid propellant and the centerport inhibitor is the same concentration on a rubber-to-rubber basis.