发明名称 BALLISTITE PROPELLANT
摘要 development of rocket propellants; rocket systems with optical guidance. SUBSTANCE: ballistite propellant contains, mas.%: nitroglycerin, 29.5-32.9; octogen, 7.0-11.0; industrial oil, 0.5-1.0; centralite, 0.9-1.3; diphenylamine, 0.2-0.5; commercial carbon, 0.2-1.1; lead-and- copper complex of phthalic acid, 1.5-4.2; calcium carbonate, 0.4-2.3; dinitrotoluene, 2.0-5.2; zinc stearate, 0.02-0.08; and nitrocellulose, the balance. EFFECT: enhanced efficiency of rocket systems provided with charges of such propellant. 1 dwg, 1 tbl
申请公布号 RU2191765(C1) 申请公布日期 2002.10.27
申请号 RU20010111138 申请日期 2001.04.23
申请人 "NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT POLIMERNYKH MATERIALOV";FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE;PERM ZD IM S M KIROVA 发明人 IBRAGIMOV N.G.;ZHURAVLEVA L.A.;PECHENKINA M.A.;VSHIVKOVA V.I.;MOLCHANOV V.F.;TALALAEV A.P.;OKHRIMENKO EH.F.;KUZ'MITSKIJ G.EH.;FEDCHENKO N.N.
分类号 C06B25/22;C06D5/06;(IPC1-7):C06B25/22 主分类号 C06B25/22
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