| 轻小型再入飞行器发展研究 |
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| 引用本文： | 耿云飞,高洁,陆亚东,李齐.轻小型再入飞行器发展研究[J].航天器工程,2014,23(6):99-104. |
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| 作者姓名： | 耿云飞 高洁 陆亚东 李齐 |
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| 作者单位： | 北京空间飞行器总体设计部,北京,100094 |
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| 摘 要： | 为实现深空探测无人取样返回任务,目前国外普遍采用轻小型化返回飞行器,并已取得较大成功。文章概述了星尘号、起源号和隼鸟号3个典型深空高速再入返回器的情况及技术特点,在此基础上分析了我国开展轻小型再入返回器研究的技术需求及发展建议,指出需要在高速再入返回气动技术、轻小型高速再入返回热防护技术、超声速降落伞回收技术、轻小型机构与综合电子技术等方面进行突破。
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| 关 键 词： | 轻小型 再入 飞行器 任务特点 |
Demonstration of Light Reentry Vehicle Development |
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| GENG Yunfei,GAO Jie,LU Yadong,LI Qi.Demonstration of Light Reentry Vehicle Development[J].Spacecraft Engineering,2014,23(6):99-104. |
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| Authors: | GENG Yunfei GAO Jie LU Yadong LI Qi |
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| Institution: | 1.Beijing Institute of Spacecraft System Engineering, Beijing 100094, China) |
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| Abstract: | The main space countries employ light reentry vehicles to implement deep space exploration and have gain success.The general situations of Stardust,Genesis and Hayabusa reentry capsules are summarized.Then the technology requirements are analyzed for our deep space light reentry vehicles.The article points out that the aerodynamics technology for hypervelocity reentry,thermal protection technology,supersonic parachute technology,light and smart framework and electron technologies need to be broken through. |
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| Keywords: | light reentry vehicle mission characteristics |
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