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
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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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