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 US8344304(B2) 申请公布日期 2013.01.01
申请号 US20100964798 申请日期 2010.12.10
申请人 RAYTHEON COMPANY;GESWENDER CHRIS E. 发明人 GESWENDER CHRIS E.
分类号 F41G7/00;F42B15/01;G06F19/00 主分类号 F41G7/00
代理机构 代理人
主权项
地址