发明名称 DEVICE FOR SOLID PROPELLANT TEMPERATURE CONTROL OF LOADED CHARGES OF SOLID PROPELLANT
摘要 production of solid propellant charges. SUBSTANCE: the device for propellant temperature control of charges has a base and two half-bodies with a vertical longitudinal half-bodies with a vertical longitudinal joint. Each half-body is hinge-joined to the base and has a release mechanism. To provide the condition of temperature control, the device is provided with a hot water register and a fan. Openings are made in the ends of the half-body in which trays are installed for movement in the device axis on the guides on the base and providing leak- proofness in the extreme positions. It makes complete opening of the device unnecessary and guarantees a stable thermal condition. EFFECT: prevented heat loss at extraction of test samples. 2 dwg
申请公布号 RU2179703(C1) 申请公布日期 2002.02.20
申请号 RU20000120462 申请日期 2000.08.04
申请人 FEDERAL'NYJ TSENTR DVOJNYKH TEKHNOLOGIJ "SOJUZ" 发明人 ELIZAR'EVA T.M.;PALEKHA A.I.;MONAKHOV V.F.;DAVYDOV V.V.
分类号 F42B39/18;(IPC1-7):F42B39/18 主分类号 F42B39/18
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