초록 ▼

An energetic solid rocket motor propellant having one or more plateau regions of low operating pressure exponent is disclosed. The propellant is formulated from ingredients including an energetic polyoxetane, an effective amount of a plasticizer, an inorganic oxidizer in at least two discrete partic

An energetic solid rocket motor propellant having one or more plateau regions of low operating pressure exponent is disclosed. The propellant is formulated from ingredients including an energetic polyoxetane, an effective amount of a plasticizer, an inorganic oxidizer in at least two discrete particle size ranges, and a refractory oxide burn rate modifier.

대표청구항 ▼

[ What is claimed is:] [1.]1. An energetic solid rocket motor propellant having one or more plateau regions of low operating pressure exponent, said propellant being formulated from ingredients comprising:at least one energetic oxetane homopolymer, copolymer, or terpolymer;an effective amount of at

[ What is claimed is:] [1.]1. An energetic solid rocket motor propellant having one or more plateau regions of low operating pressure exponent, said propellant being formulated from ingredients comprising:at least one energetic oxetane homopolymer, copolymer, or terpolymer;an effective amount of at least one plasticizer;at least one inorganic oxidizer in at least two discrete particle size ranges; andat least one refractory oxide burn rate modifier.