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