发明名称 |
Missile steering arrangement using thrust control. |
摘要 |
<p>A reaction control system for a projectile includes two oppositely directed nozzle assemblies (20) each including a control element (24). The control elements are operated inversely by a control member (30). Each control element (24) includes lost motion means (34) to accommodate movement between a sealing end (26) and a distal end (28) thereof. <IMAGE></p> |
申请公布号 |
EP0489712(A2) |
申请公布日期 |
1992.06.10 |
申请号 |
EP19920101745 |
申请日期 |
1989.02.10 |
申请人 |
BRITISH AEROSPACE PUBLIC LIMITED COMPANY |
发明人 |
MACHELL, ANTHONY;FOULSHAM, PETER G. |
分类号 |
F02K9/88;F42B10/66 |
主分类号 |
F02K9/88 |
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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