现代防御技术2012，Vol.40Issue(4)：76-79,83,5.DOI:10.3969/j.issn.1009-086x.2012.04.014
高超声速防空导弹结构防热技术展望
Outlook of Structure Thermo Protection Technology for Hypersonic Speeding Air Defense Missile
辛玲 1于江祥 1李雨时1
作者信息
- 1. 北京电子工程总体研究所,北京100854
- 折叠
摘要
Abstract
In recent years, hypersonic air defense missile has become a hot issue studied by in military powers. Flight Mach number of such missile can reach above 8 Mach. Therefore, how to accurately determine thermal environment and make a reasonable thermo-protection design are the key technologies for developing near hypersonic air defense missile. Based on the thermal environment that hypersonic air defense missile may face and combined with the development of thermal protection materials and thermal structure researches around the world, some thermo-protection designs for hypersonic air defense missiles are proposed.关键词
高超声速/防空导弹/结构防热Key words
hypersonic speed/air defense missle/structure thermo protection分类
军事科技引用本文复制引用
辛玲,于江祥,李雨时..高超声速防空导弹结构防热技术展望[J].现代防御技术,2012,40(4):76-79,83,5.
