发明名称 SOLID PROPELLANT OF BALLISTIC TYPE
摘要 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
申请公布号 RU2203872(C2) 申请公布日期 2003.05.10
申请号 RU20010118489 申请日期 2001.07.04
申请人 "NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT POLIMERNYKH M 发明人 IBRAGIMOV N.G.;OKHRIMENKO EH.F.;TALALAEV A.P.;GACHEGOVA L.G.;ALIKIN V.N.;PECHENKINA M.A.;KOZ'JAKOV A.V.;KUZ'MITSKIJ G.EH.
分类号 C06B25/26;C06D5/06 主分类号 C06B25/26
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