发明名称 Missile jet vane control system and method
摘要 A jet vane control system and method for a missile in which the system is compact, rugged, lightweight and detachably connected to the aft end of a missile. The system provides for very quick pitch over and roll control during launch. The system then detaches from the missile so as not to burden the missile during its flight to target. The vanes of the system are divided into quadrants, each having its own, mounting support and gear train assembly. Each vane is also connected through a, detachable coupling to the steering control system of the missile such that actuation of the steering control system simultaneously actuates the jet vane control system.
申请公布号 US5806791(A) 申请公布日期 1998.09.15
申请号 US19950452211 申请日期 1995.05.26
申请人 RAYTHEON COMPANY 发明人 HATALSKY, WILLIAM M.;FACCIANO, ANDREW B.;HAIGHT, STEPHEN D.;JOHNSON, SEAN A.;JORDAN, ASZETTA D.
分类号 F02K9/80;F02K9/90;F02K9/97;F42B10/64;(IPC1-7):F42B10/00;F02K1/00 主分类号 F02K9/80
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