发明名称 |
Gas jet steering device and method missile comprising such a device |
摘要 |
A steering device comprising an annular element having N exhaust nozzles and a rotary element disposed coaxially inside said annular element; the rotary element comprising M gas passageways may be positioned in MN discrete directions so as to provide a transverse thrust force orientated in one of the steering planes.
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申请公布号 |
US4463921(A) |
申请公布日期 |
1984.08.07 |
申请号 |
US19820370100 |
申请日期 |
1982.04.20 |
申请人 |
THOMSON-BRANDT |
发明人 |
METZ, PIERRE |
分类号 |
B64G1/26;B64C15/14;(IPC1-7):F42B15/02 |
主分类号 |
B64G1/26 |
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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