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
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