节点文献
典型采样返回探测器的进入减速着陆系统分析
Entry,Descent,and Landing System Analysis of Typical Sampling & Return Capsules
【摘要】 通过对典型的采样返回探测器(星尘号和起源号)的研究分析,总结归纳了采样返回探测器进入减速着陆系统的特点,特别是对探测器的气动外形布局、返回轨道设计、防热材料选择、降落伞系统设计等进行了分析,可以为下一步开展月球采样返回任务提供一定的参考。
【Abstract】 Through analyzing the typical sampling and return capsule(Stardust and Genesis),the characteristics of the Entry,descent,and landing system are summarized in the paper. The technologies of the entry,descent,and landing system are studied in detail,including capsule aerodynamic configuration,trajectory design,thermal protection system,parachute system design and so on. It can provide some references to making further study of the Lunar sampling and return mission in the future.
【关键词】 月球探测;
采样返回;
进入减速着陆系统;
分析;
【Key words】 lunar exploration; sampling and return; entry,descent,and landing system(EDL); analysis;
【Key words】 lunar exploration; sampling and return; entry,descent,and landing system(EDL); analysis;
【基金】 国家重大科技专项工程
- 【文献出处】 航天器工程 ,Spacecraft Engineering , 编辑部邮箱 ,2010年05期
- 【分类号】V476
- 【被引频次】5
- 【下载频次】148