首页> 外国专利> 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

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

机译:用于固体推进剂火箭发动机的中心端口抑制剂,包括其的固体推进剂火箭发动机以及抑制固体推进剂火箭发动机的中心端口的方法

摘要

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.
机译:公开了一种用于固体推进剂火箭发动机的可倾倒的不透明中心孔及其应用方法。用于固体推进剂火箭发动机的可倾倒的中心端口抑制剂具有包含预聚物和固化剂的固化系统。将预聚物和固化剂结合以形成可倾倒的聚合物粘合剂,该粘合剂固化成无定形固体。可倾倒的中枢抑制剂还包括不透明剂。可倾倒的中心端口抑制剂还可包含增塑剂。增塑剂,预聚物和固化剂优选是与固体推进剂结合使用的相同类型。

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