发明名称 |
Articulated nose missile control actuation system |
摘要 |
A missile nose is tiltable and rotatable relative to a missile body through the action of an actuator system. In an exemplary embodiment, the actuator systems uses two electro-mechanical actuators mounted co-axially and having the output shaft of one actuator fed through the shaft of the other. One of the actuators controls a tilt angle between a longitudinal axis of the body and a longitudinal axis of the nose. The other actuator rotates the nose about the longitudinal axis of the body. A method of steering a missile includes using the actuator system to maintain the missile nose pointed at a target or other desired destination.
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申请公布号 |
US6364248(B1) |
申请公布日期 |
2002.04.02 |
申请号 |
US20000610924 |
申请日期 |
2000.07.06 |
申请人 |
RAYTHEON COMPANY |
发明人 |
SPATE WAYNE V.;ADAMS ROBERT J.;WILLIAMS DONALD P. |
分类号 |
F42B10/62;(IPC1-7):F42B10/26 |
主分类号 |
F42B10/62 |
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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