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空间站充气式下载系统的概念研究
引用本文:夏刚,董扬彪,秦子增.空间站充气式下载系统的概念研究[J].航天返回与遥感,2005,26(1):5-9.
作者姓名:夏刚  董扬彪  秦子增
作者单位:国防科技大学航天与材料工程学院,长沙,4100073
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。

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
文章编号:1009-8518(2005)01-0005-05
修稿时间:2004年11月5日

Conceptual Research on the Spacelab Inflatable Download System
Xia Gang,Dong Yangbiao,Qin Zizeng.Conceptual Research on the Spacelab Inflatable Download System[J].Spacecraft Recovery & Remote Sensing,2005,26(1):5-9.
Authors:Xia Gang  Dong Yangbiao  Qin Zizeng
Abstract: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.
Keywords:inflatable structures  Inflatable re-entry and descent technology (IRDT)  Space station  Aerospace recovery  Atmospheric re-entry  Download system
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