首页> 外文会议>Theory and practice of energetic materials >RESEARCH OF LASER IGNITION SYSTEM USED IN SOLID ROCKET MOTOR
【24h】

RESEARCH OF LASER IGNITION SYSTEM USED IN SOLID ROCKET MOTOR

机译:固体火箭发动机激光点火系统的研究

获取原文
获取原文并翻译 | 示例

摘要

A practical laser ignition system for the ground test of solid rocket motor is developed successfully. This system adopts solid Nd: YAG laser as a power source and optical fiber cables as energy conveyors to initiate the laser initiated detonators ( LIDs) first, the through bulkhead initiators ( TBIs) are detonated second, and finally the igniter of solid rocket motor is ignited. Two kinds of LIDs and TBIs design are regarded as the most suitable choice for the ignition according to a lot of tests. The system provides outstanding safety by utilizing a mechanical laser shuttle for positive laser interruption and high reliability by using redundant optical fiber cables. The design, description, performance, development status and the main problems to be done in the future are reported.
机译:成功开发了一种用于固体火箭发动机地面试验的实用激光点火系统。该系统采用固态Nd:YAG激光作为动力源,光缆作为能量输送带,首先引爆激光引爆雷管(LID),其次引爆穿墙式引爆器(TBI),最后引爆固体火箭发动机的点火器。被点燃。根据大量测试,两种LID和TBI设计被认为是点火的最合适选择。该系统通过使用机械激光穿梭机来实现正向激光中断,并通过使用冗余光纤电缆来确保高可靠性,从而提供了出色的安全性。报告了设计,描述,性能,开发状态以及将来要完成的主要问题。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号