发明名称 METHODS AND APPARATUS FOR MISSILE AIR INLET
摘要 Methods and apparatus for delivering a missile may operate in conjunction with a missile comprising an outer skin. The missile may be configured in a closed position and an open position. In the open position, an aperture is opened in the outer skin, for example to supply air to an air-breathing engine. In the closed position, the aperture is closed.
申请公布号 WO2008091362(A2) 申请公布日期 2008.07.31
申请号 WO2007US72233 申请日期 2007.06.27
申请人 RAYTHEON COMPANY;GESWENDER, CHRIS, E. 发明人 GESWENDER, CHRIS, E.
分类号 F42B12/00 主分类号 F42B12/00
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