摘要
空间站充气式下载系统 (IDS)是在俄罗斯充气式再入与降落技术 (IRDT)基础上发展起来的一种新概念航天回收技术。详细介绍了IDS基本概念和工作原理 ,通过与传统降落伞回收方式的比较 ,总结了该技术的特点。讨论了该技术对结构、轨道、气动力、气动热、热防护层等关键子系统的设计需求。归纳了国外研究现状及发展趋势 ,分析了航天和军事领域的应用前景。
An innovative aerospace recovery technology known as Inflatable Download System (IDS) is based on the Russian Inflatable Re-entry and Descent Technology(IRDT). Basic concepts and mechanisms of the IDS are provided here in detail. Main characteristics of the IDS are concluded through comparison with the traditional parachute recovery methods. Main subsystem technologies are outlined, e.g. structure, trajectory, aerodynamics, aeroheating and thermal protection system. With the analysis of its state-of-art and trend, potential applications of IDS in military and aerospace are introduced and evaluated.
出处
《航天返回与遥感》
2005年第1期5-9,23,共6页
Spacecraft Recovery & Remote Sensing
关键词
充气式结构
充气式再入与降落技术
空间站
航天回收
大气再入
下载系统
inflatable structures Inflatable re-entry and descent technology (IRDT) Space station Aerospace recovery Atmospheric re-entry Download system
