发明名称 |
Ram air steering system for a guided missile |
摘要 |
An opening in the nose of a missile allows entry of ram air during missile flight to a central chamber. Oppositely oriented steering jets are interconnected with the aft end of the central chamber and escaping ram air provides lateral steering thrust forces. A movable diverting means controls the direction that the escaping ram air is diverted and thereby controls the steering forces.
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申请公布号 |
US4522357(A) |
申请公布日期 |
1985.06.11 |
申请号 |
US19830489662 |
申请日期 |
1983.01.19 |
申请人 |
FORD AEROSPACE & COMMUNICATIONS CORP. |
发明人 |
BAINS, WILLIAM R.;SUMRALL, CALHOUN W. |
分类号 |
B64C15/00;F41G7/00;F42B10/60;(IPC1-7):F41G7/00;B64C21/08 |
主分类号 |
B64C15/00 |
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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