空军工程大学学报（自然科学版）2013，Vol.14Issue(2)：5-8,4.DOI:10.3969/j.issn.1009-3516.2013.02.002
内装式运载火箭空中发射过程的安全性分析
Study on Safety of Carrier Aircraft during Launch Vehicle Separation from Aircraft
摘要
Abstract
The safety of carrier aircraft and rocket is the foundation of inner air launch system. Linear theories with small disturbance and time-domain method are applied to study the stability^ flying quality and safety during separation in cabin, and some ways are brought forward to improve flying quality. It is considered that rocket is likely to hit aircraft and the effect of carrier aircraft's pitch angle and rocket's location are simulated by using the kinematics equation of rocket. Through explosion comparability theory, the influence of rocket explosion wave on aircraft and pilot is taken into account and safe distance is obtained. The results of qualitative and quantitative analyses provide a theoretical basis for the application of inner air launch system.关键词
运载火箭/内装式空中发射/安全性/时域法/爆炸相似律Key words
rocket/ air launch/safety/ time-domain method/ explosion comparability theory分类
航空航天引用本文复制引用
张艳华,李华星,张登成,胡孟权,屈亮..内装式运载火箭空中发射过程的安全性分析[J].空军工程大学学报（自然科学版）,2013,14(2):5-8,4.基金项目
航空科学基金资助项目(20110596007) （20110596007）
