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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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