-
公开(公告)号:US20090194632A1
公开(公告)日:2009-08-06
申请号:US12024532
申请日:2008-02-01
CPC分类号: F42B15/01
摘要: Methods and apparatus for a missile having an external system operate in conjunction with an airframe and a fluid transfer system. The airframe includes an interior surface defining a substantially enclosed internal chamber. The fluid transfer system selectively connects the internal chamber to the external system, for example to provide pressurant or coolant to the external system.
摘要翻译: 具有外部系统的导弹的方法和装置与机身和流体传输系统一起操作。 机身包括限定基本封闭的内部腔室的内表面。 流体传输系统选择性地将内部室连接到外部系统,例如以向外部系统提供加压或冷却剂。