发明名称 |
Missile launch apparatus |
摘要 |
A deployment mechanism for shielding and deploying an optical fibre (14) on the launch of a missile (10) incorporating a rigid, elongate guide (30) running along the outer surface of the missile (10) and to which a portion of the fibre is releasably attached. An end of the fibre is attached to an anchorage point 18 on the launch tube. On launch, the fibre (14) peels away from the guide without sustaining any excessive load before the remaining fibre (14) pays out from a spool (12) mounted within the missile (10). |
申请公布号 |
GB2434190(A) |
申请公布日期 |
2007.07.18 |
申请号 |
GB19950000769 |
申请日期 |
1995.01.16 |
申请人 |
BRITISH AEROSPACE PUBLIC LIMITED COMPANY;MATRA BAE DYNAMICS;MBDA UK LIMITED |
发明人 |
RICHARD W GRAINGE;ANTHONY MACHELL;ANTHONY J MANN |
分类号 |
F42B15/04;F41G7/30;F41G7/32 |
主分类号 |
F42B15/04 |
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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