发明名称 ROCKET ENGINE IGNITER
摘要 rocketry; engines. SUBSTANCE: igniter of rocket engine solid propellant charge has pyrotechnical cartridge and igniter whose housing is made equidistant to surface of seat in engine. Igniter housing is made of polymeric film in form of three-dimensional unit with cavity in housing. Cavity accommodates cartridge divider which has central blind channel and side radial channels. Cross sizes of cavity are either equal to or slightly less than cross sizes of divider. Radial channels of divider are mutually opposite. EFFECT: provision of compact design of igniter with convenience of arrangement and fastening in rocket engine and improved reliability of operation. 2 cl, 2 dwg
申请公布号 RU2185522(C1) 申请公布日期 2002.07.20
申请号 RU20010104249 申请日期 2001.02.13
申请人 GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "NAUCHNO-IS;FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE;PERM ZD IM S M KIROVA;FEDERALNOE GUP 发明人 TALALAEV A.P.;KOZ'JAKOV A.V.;MOLCHANOV V.F.;CHURAKOV V.V.;ALIKIN V.N.;KUZ'MITSKIJ G.EH.
分类号 F02K9/95;(IPC1-7):F02K9/95 主分类号 F02K9/95
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