发明名称 TEST BENCH FOR ROCKET ENGINES WITH THIN-WALL NOZZLES
摘要 FIELD: engines and pumps.SUBSTANCE: proposed test bench comprises altitude chamber, exhaust diffuser, ring ejector and ejecting working medium source. Said ejecting working medium source is composed of steam generator composed by jacket enclosing the diffuser. Diffuser inlet is communicated with coolant feed line while its outlet is connected with circular ejector. Test bench is furnished with nozzles arranged in circular ejector. Said nozzles have software-destructive cases.EFFECT: simulation of high-altitude conditions, higher safety.2 cl, 3 dwg
申请公布号 RU2513063(C1) 申请公布日期 2014.04.20
申请号 RU20130107902 申请日期 2013.02.21
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "ISKRA" 发明人 NAZARTSEV ALEKSANDR ALEKSANDROVICH;PATRULIN SERGEJ VLADIMIROVICH
分类号 F02K9/96;G01M15/14 主分类号 F02K9/96
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