摘要
本文通过简化的假设及严格的推导，给出了一套用于再入飞行器总体方案论证阶段的热环境参数的定性分析和定量计算方法，适于总体设计人员在总体参数估算中应用，也可以作为总体人员定性分析再入特性时使用。
A set of methods of qualitative analysis and quantitative calculation of heat environment parameters which is used in system definition phase of re-entry vehicle is given in this paper through simplified hypothesis and strict derivation. It can be used in estimating system parameters and analysing re-entry characteristics qualitatively.
出处
《导弹与航天运载技术》
1994年第4期31-38,共8页
Missiles and Space Vehicles
关键词
再入飞行器
热环境
数值计算
Reentry vehicle, Thermal environment, Numerical calcalation.
