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[1]刘 川,刘 俊,邱 鑫,等.火星探测器推进系统初步设想[J].火箭推进,2014,40(02):44-48.
　LIU Chuan,LIU Jun,QIU Xin,et al.Preliminary design of propulsion system for Mars exploration[J].Journal of Rocket Propulsion,2014,40(02):44-48.
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火星探测器推进系统初步设想

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 40 期数: 2014年02期 页码: 44-48 栏目: 研究与设计 出版日期: 2014-04-28
Title:
Preliminary design of propulsion system for Mars exploration
作者:
刘 川; 刘 俊; 邱 鑫; 林庆国
上海空间推进研究所，上海 201112
Author(s):
LIU Chuan;  LIU Jun;  QIU Xin;  LIN Qing-guo
Shanghai Institute of Space Propulsion, Shanghai 201112, China
关键词:
火星探测; 推进系统; 初步设计; 关键技术
Keywords:
Mars exploration;  propulsion system;  preliminary design;  key technology
分类号:
V434-34
文献标志码:
A
摘要:
火星探测是深空探测的重要内容之一，全面了解和掌握火星探测器的特点对进行火星探测具有重要意义。本文分析了国外火星探测器推进系统的系统组成和工作原理，介绍了我国火星探测器推进系统的初步设计方案，结合工程应用现状，提出了火星探测器推进系统的关键技术。
Abstract:
Mars Exploration is an important content of deep space exploration. It is significant to understand and master the characteristics of Mars lander for Mars exploration. The system composi- tion and working principle of the propulsion systems of foreign Mars landers are analyzed in this paper. The preliminary design scheme of Mars lander propulsion system in China is introduced. According to the engineering status, the key technologies associated with Mars lander propulsion system are presented.

参考文献/References:

[1]王海涛, 付丽璋, 蒋万松. 凤凰号火星探测器着陆过程[J]. 航天返回与遥感, 2009, 30(3): 8-15.
[2]褚英志, 李秀伟, 周晓东. 火星探测关键技术分析[J]. 测试技术学报, 2007, 21（增刊）: 63-66.
[3]MORRISEY D C. Historical perspective-Viking Mars lan- der propulsion, AIAA-1989-2391[R]. USA: AIAA, 1989.
[4]BARBE T J, PICHA F Q. In-flight propulsion system cha- racterization for both Mars exploration rover spacecraft, AIAA-2004-3695[R]. USA: AIAA, 2004.
[5]D'AMARIO L A. Mars exploration rovers navigation re- sults, AIAA-2004-4980[R]. USA: AIAA, 2004.
[6]PLEMMONS D, WILCHER K. Spectroscopic plume ana- lysis of the Phoenix Mars Lander hydrazine mono- propellant thrusters, AIAA-2007-5706[R]. USA: AIAA, 2007.
[7]DESAI P N. Entry, descent, and landing performance of the Mars Phoenix Lander, AIAA-2008-7346[R]. USA: AIAA, 2008.
[8]DAWSON Matt. Monopropellant hydrazine 700 lbf thrott- ling terminal descent engine for Mars science laboratory, AIAA-2007-5481 [R]. USA: AIAA, 2007.
[9]PARIS A D, NOVAK K S, KELLY F P, et al. Overview of the Mars science laboratory cruise phase system thermal vacuum test, AIAA-2010-6189[R]. USA: AIAA, 2010.
[10]MCRIGHT P, POPP C, PIERCE C, et al. Confidence testing of shell-405 and S-405 catalysts in a mono- propellant hydrazine thruster, AIAA-2005-3952[R]. USA: AIAA, 2005.

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备注/Memo

收稿日期：2013-12-26；修回日期：2014-01-20 作者简介：刘川（1986—），男，硕士，研究领域为空间飞行器推进系统

更新日期/Last Update: 1900-01-01