FIELD: development of high-energy fast-burning solid propellants of ballistic type ( double-base propellants ). SUBSTANCE: in agreement with invention solid propellant of ballistic type contains nitroglycerin, stabilizer of chemical stability ( centralite and diphenylamine ), technological additives ( industrial oil and zinc stearate ), burning stabilizer ( calcium carbonate ), burning modifier ( lead hydroxide and technical carbon ), colloxilin, synthetic latex, fluroplastic, polymethyl or polyethylsiloxane fluids, noncomminuted cellulose with nitrogen content of 13% or above. EFFECT: development of high-energy fast-burning solid propellant of ballistic type demonstrating high operational safety. 1 tbl
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Authors
Dates
2003-05-10—Published
2001-07-04—Filed