| 发明名称 |
Control device for missiles |
| 摘要 |
The invention relates to a control device for a missile which consists of a jetpipe which can rotate about its longitudinal axis, to which compressed gas is applied and which has a radially directed jet exhaust, and of an aerodynamic body which corresponds to the jetpipe.
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| 申请公布号 |
DE3227336(A1) |
申请公布日期 |
1984.02.02 |
| 申请号 |
DE19823227336 |
申请日期 |
1982.07.22 |
| 申请人 |
MESSERSCHMITT-BOELKOW-BLOHM GMBH |
发明人 |
RIEGER,ULRICH,DIPL.-ING. |
| 分类号 |
B64C15/14;(IPC1-7):B64C15/14 |
主分类号 |
B64C15/14 |
| 代理机构 |
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