发明名称 ORIENTABLE ROCKET-MOTOR SYSTEM
摘要 A system allowing for the tilting of the rocket motor such that, in the tilted position, the centre of the nozzle is located at least approximately on the neutral orientation axis of said rocket motor.
申请公布号 EP2989314(B1) 申请公布日期 2017.03.08
申请号 EP20140725212 申请日期 2014.04.22
申请人 Airbus Safran Launchers SAS 发明人 RUFFINO Fabrice;FAURE Benjamin
分类号 F02K9/80;F02K9/56;F02K9/84 主分类号 F02K9/80
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