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Improvements in airborne missile launcher.

机译:机载导弹发射器的改进。

摘要

An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
机译:一种用于空中发射管载导弹的机载导弹发射器,包括中央支撑框架,该中央支撑框架具有用于可拆卸地附接到飞机或其他发射平台的附接装置,该中央框架构件的每侧均具有发射管鞍形支撑组件具有快速可拆卸的夹紧装置的框架部件和用于快速将发射管定位和固定到位的对准导向器,以及具有自动连接装置的对准导向装置,该自动连接装置用于在将电子控制系统和冷却剂气体夹紧到位后将其自动连接到发射管组件。空气动力学壳体包围支撑结构,并包括快速释放盖,该快速释放盖用于接近管夹组件以装载和卸载发射管。

著录项

  • 公开/公告号ES515719A0

    专利类型

  • 公开/公告日1983-08-16

    原文格式PDF

  • 申请/专利权人 GENERAL DYNAMICS CORPORATION POMONA DIVISION.;

    申请/专利号ES19820515719

  • 发明设计人

    申请日1982-09-15

  • 分类号F41F3/06;

  • 国家 ES

  • 入库时间 2022-08-22 10:46:56

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