| 月球着陆器方案概念设想 |
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| 引用本文： | 彭兢,柳忠尧,张熇.月球着陆器方案概念设想[J].航天器工程,2008,17(1):18-23. |
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| 作者姓名： | 彭兢 柳忠尧 张熇 |
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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： | 文章针对月球软着陆任务，对整个飞行过程进行了描述，简介了着陆器的主要特性和系统总体设计，并对其中主要的几个关键分系统的特点和适应软着陆任务的方案设想进行了描述，包括结构、缓冲机构、导航与控制、推进、测控通信、供配电、热控等。
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| 关 键 词： | 月球着陆器 轨道 概念设想 |
| 文章编号： | 1673-8748(2008)01-0018-06 |
| 修稿时间： | 2007年10月19 |
Conceptual Design of A Lunar Lander |
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| PENG Jing,LIU Zhongyao,ZHANG He.Conceptual Design of A Lunar Lander[J].Spacecraft Engineering,2008,17(1):18-23. |
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| Authors: | PENG Jing LIU Zhongyao ZHANG He |
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| Institution: | PENG Jing, LIU Zhongyao, ZHANG He (Beijing Institute of Spacecraft System Engineering,Beijing 100094,China) |
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| Abstract: | For a lunar soft landing mission,the flight profile of the landing mission is described in this paper.After a brief introduction to key parameters and system design of the lander,more technical information about conceptual design of subsystems such as structure,bumper mechanism,propulsion,navigation and control,power supply and thermal control is given as well. |
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| Keywords: | lunar lander orbit conceptual design |
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