发明名称 Steerable missile
摘要 <p>The guidable missile has a tubular body (1) and a tilt-movable missile nose (2) attached at the body, where an actuator is formed by multiple electromagnets (30,34). The missile nose is provided with radially extending flow-like ribs running in longitudinal direction. The electromagnets are operated against a force of an arranged elastic resetting element (39,39'), particularly a reset spring.</p>
申请公布号 EP2418454(A2) 申请公布日期 2012.02.15
申请号 EP20110006540 申请日期 2011.08.09
申请人 LFK-LENKFLUGKOERPERSYSTEME GMBH 发明人 GLEICH, PETER
分类号 F42B10/62;F42B10/22;F42B10/46 主分类号 F42B10/62
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