发明名称 ROCKET ENGINE SOLID PROPELLANT CHARGE
摘要 FIELD: rocketry. SUBSTANCE: solid propellant charge for rocket engine consists of series-mounted grains with metal reinforcement member placed in arch. Reinforcement member in each propellant grain is made of high porosity material of three-dimensional structure of different thermal conductivity, for instance, copper, nickel, and is filled up with propellant of one type. Invention makes it possible to form solid propellant charge with multiple step control of engine thrust. EFFECT: provision of high operation reliability and standard technology of manufacture of charges. 2 dwg
申请公布号 RU2195568(C2) 申请公布日期 2002.12.27
申请号 RU20010106839 申请日期 2001.03.12
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE;FEDERALNOE GUP 发明人 ALIKIN V.N.;KUZ'MITSKIJ G.EH.;FEDCHENKO N.N.;KOVTUN V.E.;SEMENOV V.V.
分类号 F02K9/16;(IPC1-7):F02K9/16 主分类号 F02K9/16
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