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Missile hot gas withstanding optic fiber resistance system

机译:导弹热气耐受光纤电阻系统

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
机译:用于从管子(12)热发射的导弹(10)的光纤(18)放出系统通过与一根或多根导线(24)和一根或多根并置,加强了该部分光纤以暴露于推进气体。封装在热保护护套(22)内形成所谓的引导件(20)。引导器(20)从导弹的后端(16)向外延伸,并通过柔性带(46)可释放地固定在导轨组件(32)内,柔性带(46)具有沿其纵轴延伸的穿孔线(48)。引导件(20)的外端部固定在锚定块(52)上。发射时,引导器(20)从柔性条带(46)撕开,其约束作用阻止了光纤的预分配。 <图像>

著录项

  • 公开/公告号IL97418A

    专利类型

  • 公开/公告日1995-05-26

    原文格式PDF

  • 申请/专利权人 HUGHES AIRCRAFT COMPANY;

    申请/专利号IL19910097418

  • 发明设计人

    申请日1991-03-04

  • 分类号F42B15/04;

  • 国家 IL

  • 入库时间 2022-08-22 04:19:11

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