发明名称 DIRECTIONAL CONTROL OF MISSILES
摘要 <p>Missile (10) includes one or more of barrel assemblies (11) which are displaced from the centre of gravity of missile (10). Each barrel assembly (11) includes a plurality of projectiles axially disposed within the barrel, and each projectiles is associated with a discrete propellant charge for propelling the projectile sequentially from the barrel. Each array of barrel assemblies (11) is capable of selectively firing the projectiles from selected barrels whereby missile (10) is accelerated by the reactionary force generated by said firing of projectiles and the missile is deflected onto a new course or trajectory. This enables missile (10) to be steered to intercept its target even if the target is undertaking evasive manoeuvre. Each barrel assembly (11) can include up to twelve projectiles.</p>
申请公布号 WO2001090682(A1) 申请公布日期 2001.11.29
申请号 AU2001000607 申请日期 2001.05.25
申请人 发明人
分类号 主分类号
代理机构 代理人
主权项
地址