发明名称 Exhaust assembly for missile system, and method
摘要 A system, device and method provide an exhaust assembly adapted for use with a mass ejection drive system to produce rotational torque about the principle axis of the drive system. Representative features generally include a vane suitably configured to at least partially engage a mass ejecta stream to apply a net rotational torque about the principal axis of the drive system, and a tailfin coupled to the at least one vane. The tail fin is configured to selectively deploy from an at least partially stowed position in order to decrease the application of net rotational torque about the principal axis of the drive system.
申请公布号 US7728266(B2) 申请公布日期 2010.06.01
申请号 US20060549223 申请日期 2006.10.13
申请人 RAYTHEON COMPANY 发明人 MELKERS EDGAR R.;EISENTRAUT RUDY;STRASSMAN DORON
分类号 F42B15/01 主分类号 F42B15/01
代理机构 代理人
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