发明名称 PROJECTILE
摘要 A projectile (100) is provided for operating at least in a launch phase and in a post-launch phase. The projectile includes a projectile body (10), a projectile head (50), and a support structure (80). The projectile head is non-rigidly mounted to the projectile body via a joint structure (70). The support structure is configured for selectively supporting the projectile head with respect to the projectile body in a load bearing relationship independently of the joint structure during at least a portion of the launch phase, and for selectively terminating the support during at least a portion of the post-launch phase. A method for operating a projectile and a method for retrofitting a projectile are also provided.
申请公布号 EP2659219(A2) 申请公布日期 2013.11.06
申请号 EP20110815638 申请日期 2011.12.26
申请人 ISRAEL AEROSPACE INDUSTRIES LTD. 发明人 LEVY, BENJAMIN;HAYAT, ABRAHAM
分类号 F42B10/46;F42B10/64;F42B15/01;F42B30/10 主分类号 F42B10/46
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