发明名称 STOPPER OF JET ENGINE WITH LOW TRACTION
摘要 A thruster cap that is installed on its nozzle is a construction made of filtering material. At preservation of function of protection of rocket engine against contamination and mechanical damages at transportation, keeping, routine maintenance, the cap provides possibility of evacuation of mains of propulsion unit before filling those with components of rocket fuel in process of flight by means of the rocket engine.
申请公布号 UA82092(C2) 申请公布日期 2008.03.11
申请号 UA20050010163 申请日期 2005.10.28
申请人 &LDQUO,M.YANHEL &LDQUO,PIVDENNE&RDQUO, DESIGN OFFICE&RDQUO,, STATE ENTERPRISE 发明人 ANISCHENKO VIACHESLAV MYKHAILOVYCH;DOBROHORSKYI VIKTOR ANTONOVYCH;KOSHKIN MYKHAILO IVANOVYCH;KOMEKO YEGOR MYKYTOVYCH;UDOVIKA TETIANA MYKOLAIVNA
分类号 F02K1/00 主分类号 F02K1/00
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