发明名称 Modular missile and method of assembly
摘要 A modular missile assembly includes a pair of modules which are separately transported and handled until just prior to firing, when they are coupled together. A forward payload-carrying module includes a forward canister which encloses a missile payload section, for example, consisting of a penetrator rod, fins, and ancillary sub-assemblies. An aft booster module includes a missile propulsion section, encased in an aft canister. Prior to firing, suitable forward and aft modules are selected, are individually loaded into a launch tube, and are coupled together. In this coupling the missile payload section and the missile propulsion section are coupled together to form a missile, and the forward and aft canisters are likewise coupled together to form a combined canister assembly. Division of the missile into separate payload and booster modules facilitates handling as compared to unitary missiles. The modular design also allows increased flexibility.
申请公布号 US6568330(B1) 申请公布日期 2003.05.27
申请号 US20010802717 申请日期 2001.03.08
申请人 RAYTHEON COMPANY 发明人 KAISERMAN MICHAEL J.;RODACK MICHAEL T.;SCHNEIDER ARTHUR J.;SPATE WAYNE V.;WEESNER JENNIFER B.;WINETROBE STANTON L.
分类号 F41F3/00;F42B5/38;F42B15/10;F42B15/36;(IPC1-7):F42B15/10 主分类号 F41F3/00
代理机构 代理人
主权项
地址