Composite double base propellant with HMX oxidizer

摘要

1. A solid propellant composition comprising, by weight, 50 percent cyclotetramethylene tetranitramine, 17.7 percent nitrocellulose, 22.1 percent nitroglycerin, 5.2 percent triacetin, 0.5 percent diethylphthalate, 2.0 percent basic lead beta resorcylate, 2.0 percent basic cupric salicylate, 0.5 percent 2-nitrodiphenylamine, and 0.02 percent carbon black.