美澳马赫数7+乘波体高超声速飞行试验分析  

Analysis on the Hypersonic Flight Test of Mach 7 + Waverider Vehicle Developed by US and Australia

作　　者：张灿 胡冬冬[1] Zhang Can;Hu Dongdong(Beijing HIWING Scientific and Technological Information Institute, Beijing 100074, China)

机构地区：[1]北京海鹰科技情报研究所,北京100074

出　　处：《战术导弹技术》2017年第5期12-15,21,共5页Tactical Missile Technology

摘　　要：基于美澳合作的高超声速国际飞行研究试验(HIFiRE)项目近期公布的HIFiRE 4高超声速飞行试验动态,全面梳理了HIFiRE项目的研究背景和目的,并对此次HIFiRE 4的试验飞行器方案、试验目标和需求、试验任务和实际情况进行了分析。根据HIFiRE 4的试验结果,结合美国高超声速武器发展现状和HIFiRE项目后续规划,对该项目进行了分析和评述。Based on the recent hypersonic flight test HIFiRE 4 of the Hypersonic International Flight Research Experimentation（ HIFiRE） program collaborated by the United States and Australia,the research background and purpose of the program are thoroughly combed,and the test aircraft design,test objective,test requirements,test tasks and practical conditions are analyzed. In combination with the development status of American hypersonic weapons and the program follow-up plan,the program is analyzed and reviewed on the basis of HIFiRE 4 test result.

关 键 词：HIFIRE 4 高超声速 飞行试验 乘波体 

分 类 号：V217[航空宇航科学与技术—航空宇航推进理论与工程]