发明名称 |
Device for guiding a missile |
摘要 |
The invention relates to a device for guiding a missile (1; 30) with a missile tip (2) and a cylindrical section (3) adjoining the tip of the missile; the device is provided with at least one control block (4; 31, 32) with exhaust openings (13-15) of corresponding nozzle bodies (10-12) arranged perpendicularly in relation to the missile's surface. In order to accomplish effective guidance, particularly of high-speed missiles (1; 30), in a simple and cost-effective manner it is proposed that the control block (4; 31, 32) be constructed with a plurality of small, fast-burning rocket motors (7-9; 33-36) that are arranged radially on the missile's periphery (1; 30) and that are ignitable in a predeterminable sequence and number.
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申请公布号 |
US5433399(A) |
申请公布日期 |
1995.07.18 |
申请号 |
US19940253036 |
申请日期 |
1994.06.02 |
申请人 |
RHEINMETALL GMBH |
发明人 |
BECKER, WILFRIED;GROSSWENDT, WERNER;SCHWENZER, MICHAEL |
分类号 |
F41G9/00;F42B10/00;F42B10/60;F42B10/66;F42B15/01;(IPC1-7):F42B15/01 |
主分类号 |
F41G9/00 |
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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