期刊文献+

基于火箭橇的机载弹药制动冲脱试验技术 被引量:3

The Technology of Braking and Inertial Running out Test for Airborne Ammunition Based on Rocket-sled
下载PDF
导出
摘要 简要介绍了弹药制动冲脱试验原理及国内外现状,针对我国上舰机载弹药制动冲脱试验方法和标准的不足,提出了采用火箭橇技术模拟舰上机载弹药制动冲脱试验新方法,并对该方法的原理、关键技术进行了分析和仿真计算,最后通过实例验证。结果表明该试验方法可行,能满足机载弹药制动冲脱试验要求,也可供弹药安全性研究人员参考。 This paper briefly introduces the principle of braking&inertial running out safety test and the present situation at home and abroad. In view of the shortage for the airborne ammunition to carry out braking & inertial running out safety test, a new method to simulate the braking & inertial running out safety test of ammunition on board based on rocket-sled technology is developed, and its technical principles, key technologies were analyzed and simulated, which was verified combined with test. The results show that the new test method fully satisfies the safety test requirements for the airborne ammunition, which also provide reference for the ammunition safety test researchers.
作者 李君智 解珍珍 杨江 郑宁歌 LI Junzhi;XIE Zhenzhen;YANG Jiang;ZHENG Ningge(Test and Measuring Academy of China Ordance Industry,Shaanxi Huayin 714200,China)
出处 《弹箭与制导学报》 CSCD 北大核心 2018年第3期143-146,共4页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 机载弹药 火箭橇 制动冲脱 试验 airborne ammunition rocket-sled braking&inertial running out test
  • 相关文献

参考文献1

二级参考文献6

共引文献11

同被引文献57

引证文献3

二级引证文献3

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部