| 发明名称 |
Fixed canards maneuverability enhancement |
| 摘要 |
A guidance device for projectiles has stationary canards (40) and thrusters (50) positioned on the nose (20) of the projectile (10). The thrusters (50) are initiated from remote or local sensor to provide flight maneuverability to a target.
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| 申请公布号 |
US6402087(B1) |
申请公布日期 |
2002.06.11 |
| 申请号 |
US20000613147 |
申请日期 |
2000.07.11 |
| 申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY |
发明人 |
FARINA ANTHONY;AMORUSO MICHAEL J.;TOLEDO WILFREDO |
| 分类号 |
F42B10/64;(IPC1-7):F42B10/60;F41G7/00;F42B15/01 |
主分类号 |
F42B10/64 |
| 代理机构 |
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代理人 |
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| 主权项 |
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