发明名称 SISTEMA PER EROGARE UNA FIBRA OTTICA DI COLLEGAMENTO DATI PER MISSILI.
摘要 An optical fiber (18) payout system for a missile (10) which is to be hot-launched from a tube (12) reinforces that part of the fiber to be exposed to propulsion gases by juxtaposing with one or more wires (24) and encasing within a thermally protective sheath (22) forming a so-called leader (20). The leader (20) extends outwardly of the missile aft end (16) and is releasably secured within a rail assembly (32) by a flexible strip (46) having a line of perforations (48) extending along its longitudinal axis. The outer end portion of the leader (20) is secured to an anchor block (52). On launch, the leader (20) tears loose from the flexible strip (46), the restraining action of which prevents optical fiber predispensing. <IMAGE>
申请公布号 ITRM910197(A1) 申请公布日期 1991.09.29
申请号 IT1991RM00197 申请日期 1991.03.26
申请人 HUGHES AIRCRAFT COMPANY 发明人 PETERSON STANLEY P.D.;REDFORD GARY R.;SCHOTTER DANIEL K.
分类号 B65H57/18;F41F3/00;F41G;F41G7/32;F42B15/00;F42B15/04;G02B6/00;G02B6/44 主分类号 B65H57/18
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