AFRL高超声速试验低弹道发射系统试验窗口分析  

Test Window Research on AFRL Suppressed Trajectories Launch Vehicle Systems for Hypersonic Testing

作　　者：牛文[1] 李文杰[1] 叶蕾[1] 侯德飞 

机构地区：[1]北京海鹰科技情报研究所,北京100074 [2]空军装备部军械通用装备部,北京100843

出　　处：《战术导弹技术》2014年第5期1-5,共5页Tactical Missile Technology

摘　　要：主要对美国空军研究实验室针对美国空军2014财年"高超声速试验低弹道发射系统"的小型探索性研究项目提出高超声速试验窗口需求进行了情报研究,重点关注了其推进与动力、边界层、气动热、火箭返回等试验窗口形式,并对美国空军针对相关发射系统所提出的要求进行了分析。认为美国空军不仅希望改善现有发射能力,还希望可以借此获取高超声速作战能力。An analysis is accomplished according to the AFRL＇ s test window research due to US Air Force＇ Launch Vehicle Systems Intended to Execute Suppressed Trajectories for Hypersonic Testing program, special attention has been paid to the area of propulsion, boundary layer, aerothermodynamics and rocket back, as well as the lauch system requirements. A conclusion can be drawn that the US Air Force intends to improve not only the test and lauch capability, but also to form a hypersonic strike ability.

关 键 词：试验窗口 高超声速 发射系统 武器 

分 类 号：V211.7[航空宇航科学与技术—航空宇航推进理论与工程]