发明名称 |
ROCKET SOLID PROPELLANT CHARGE |
摘要 |
FIELD: rocketry. SUBSTANCE: proposed charge proper rigidly connected with housing and protective-and-fastening layer playing the part of heat protective coating and fastening layer. Protective-and-fastening layer of thickness equal to 0,1.10-2-2,5.10-2 of outer diameter of charge, being essentially sheet calendared material of basis of ethylene-propylene-diene rubber with chrysolite asbestos filler, contains also dioctyl sebacate in amount of 3-300 mass parts and para- dinitrosobenzene in amount of 2-10 mass parts. EFFECT: provision of rocket solid propellant charge reliably connected with rocket engine by one protective-and-fastening layer playing the part of heat protective coating and fastening layer. 1 tbl, 3 dwg
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申请公布号 |
RU2216641(C1) |
申请公布日期 |
2003.11.20 |
申请号 |
RU20020116944 |
申请日期 |
2002.06.24 |
申请人 |
FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE;FEDERALNOE GUP;ATERIALOV |
发明人 |
VALEEV N.S.;ZVEREVA I.G.;AMARANTOV G.N.;BARANOV G.N.;SHAMRAEV V.JA.;KUSAKIN JU.N.;TALALAEV A.P.;SOLOV'EV A.F.;KUZ'MITSKIJ G.EH.;FEDCHENKO N.N.;VRONSKIJ N.M.;MAKAROV L.B.;BULASHEVICH A.P.;EZHOV G.P.;FOKIN A.S.;OKHRIMENKO EH.F.;KOLESNIKOV V.I. |
分类号 |
F02K9/32;(IPC1-7):F02K9/32 |
主分类号 |
F02K9/32 |
代理机构 |
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代理人 |
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地址 |
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