发明名称 SPACECRAFT THERMAL CONTROL SYSTEM
摘要 FIELD: transport.SUBSTANCE: invention relates to thermal control systems of, mainly, telecommunication satellites. Thermal control system comprises closed heat carrier circulation circuit. The latter includes electrically driven pump unit, pressure accumulator, manifolds of control panels and those of radiators. Said elements are interconnected by lengths of connection pipelines with inlet and outlet flow sections complying with those of said elements. Portion of lengths of said connection pipelines feature identical equivalent ID smaller than diameters of the other parts and total length that satisfies the definite relationship.EFFECT: decreased sizes, higher reliability.1 dwg
申请公布号 RU2513321(C1) 申请公布日期 2014.04.20
申请号 RU20120142387 申请日期 2012.10.04
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "INFORMATSIONNYE SPUTNIKOVYE SISTEMY" IMENI AKADEMIKA M.F. RESHETNEVA" 发明人 KHALIMANOVICH VLADIMIR IVANOVICH;LAVROV VIKTOR IVANOVICH;KOLESNIKOV ANATOLIJ PETROVICH;DOSTAVALOV ALEKSANDR VALENTINOVICH;AKCHURIN GEORGIJ VLADIMIROVICH;KNJAZEV ALEKSANDR GRIGOR'EVICH;GORDEEV EGOR ALEKSANDROVICH;GABOV ALEKSEJ SERGEEVICH
分类号 B64G1/50;G05D1/08 主分类号 B64G1/50
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