PDF下载 分享
[1]左 坤,等.全电推商业卫星平台研究综述[J].火箭推进,2015,41(02):13-20.
　ZUO Kun,WANG Min,et al.Research overview of commercial satellite platform with all-electric propulsion system[J].Journal of Rocket Propulsion,2015,41(02):13-20.
点击复制

全电推商业卫星平台研究综述

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 41 期数: 2015年02期 页码: 13-20 栏目: 专论与综述 出版日期: 2015-07-30
Title:
Research overview of commercial satellite platform with all-electric propulsion system
作者:
左 坤1;  2; 王 敏1; 李 敏2; 汤海滨2
1. 中国空间技术研究院通信卫星事业部，北京100094； 2. 北京航空航天大学宇航学院，北京100191
Author(s):
ZUO Kun1;  2;  WANG Min1;  LI Min2;  TANG Hai-bin2
1. Institute of Telecommunication Satellite, China Academy of Space Technology, Beijing 100094, China 2. School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China
关键词:
电推进; 全电推卫星平台; 轨道转移; 位置保持; 姿态控制
Keywords:
electric propulsion;  all-electric propulsion satellite platform;  orbit transfer;  station keeping;  attitude control
分类号:
V439.4-34
文献标志码:
A
摘要:
近年来，电推进技术在空间推进中的应用越来越普遍，电推进系统主要应用于低地球轨道、同步地球轨道和星际任务三个方面。在轨道转移过程中，与传统双组元化学推进系统需消耗数吨推进剂相比，全电推进完成从地球转移轨道到同步地球轨道的变轨过程仅需数百千克推进剂，从而能够有效降低发射质量，显著提高商业效益。基于全电推进的商业卫星平台能够较大限度地提升卫星荷载比、充分发挥卫星平台承载能力，并提升卫星平台综合性能。从调研电推进系统研制和应用现状入手，介绍了国外全电推商业卫星平台开发情况，借鉴国外发展模式并结合我国电推力器研制基础和能力，提出了国内全电推商业卫星平台总体方案。
Abstract:
In recent years, the application of electric propulsion technology has been more and more popular in space propulsion, especially in missions of low earth orbit, geosynchronous earth orbit and interplanetary space. During the satellite transfer, compared with the traditional bipropellant chemical propulsion systems consuming tons of propellant, the all-electric propulsion system only consumes hundreds of kilograms propellant in the process of geosynchronous earth orbit transfer, which reduces the launch mass effectively and improves the business benefit obviously. With all-electric propulsion system, the commercial satellite platform can increase its loading ratio, give full play to its carrying capacity, and improve its combination property. Proceeding from investigation of the electric propulsion system development and application situation, the development status of the electric propulsion commercial satellites abroad is introduced. A detailed program for domestic commercial satellite platform based on all-electric propulsion is presented by conferring the development mode abroad, and in combination with the developing foundation and capability of electric propulsion in China, so that it could make a useful reference for further study in China.

参考文献/References:

[1]GOEBEL D M, KATZ I. Fundamentals of electric pro- pulsion: ion and Hall thrusters[M]. USA: John Wiley & Sons, 2008.
[2]毛根旺, 付西鹏, 陈茂林. 月球探测器电推进系统的应用研究[J]. 机械科学与技术, 2008, 27(7): 853-856.
[3]边炳秀, 魏延明. 电推进系统在静止轨道卫星平台上应用的关键技术[J]. 空间控制技术与应用, 2008, 34(1): 20-24.
[4]魏延明. 国外卫星推进技术发展现状与未来 20 年发展趋势[J]. 航天制造技术, 2011 (2): 7-12.

[5]高扬. 电火箭星际航行: 技术进展, 轨道设计与综合优化[J]. 力学学报, 2012, 43(6): 991-1019.

[6]迟惑. 全电推进卫星——商业通信卫星的新趋势[J]. 太空探索, 2012 (7): 40-42.
[7]刘江, 赵宏. 卫星电推进应用技术现状及发展[C]//全国第十二届空间及运动体控制技术学术会议论文集, 2006.
[8]谭松林, 何泽夏, 毛根旺. 国外电推进技术的新进展[J]. 火箭推进, 2001, 27(4): 13-18.
[9]张天平, 田华兵, 孙运奎. 离子推进系统用于 GEO 卫星南北位保使命的能力与效益[J]. 真空与低温, 2010 (2): 72-77.
[10]杭观荣, 康小录. 美国AEHF军事通信卫星推进系统及其在首发星上的应用[J]. 火箭推进, 2012, 37(6): 1-8.
[11]杭观荣, 邱刚, 余水淋, 等. 霍尔电推进在AEHF卫星上应用对我国霍尔电推进发展的启示[J]. 真空电子技术, 2013 (3): 5-11.
[12]崔铁民, 唐福俊. 地球静止轨道卫星平台位保应用离子电推进系统方案[J]. 真空与低温, 2009 (2): 90-94.
[13]张乾鹏, 康小录, 施晨毅, 等. 霍尔推力器束流分布特性实验研究[J]. 上海航天, 2012, 29(4): 49-53.
[14]黄建国, 赵华, 任琼英, 等. 螺旋波电推进火星超低轨道维持技术研究[C]//中国宇航学会深空探测技术专业委员会第九届学术年会论文集 (上册), 2012.
[15]CO T C. Operationally responsive spacecraft using electric propulsion[D]. Wright-Patterson Air Force Base, Ohio: Air Force Inst of Tech, 2012.
[16]BAROCELA E, CASSIDY P F. Delta-winged hybrid airship: US, 7093789 [P]. 2006-08-22.
[17]全电推进卫星余震尚存[J]. 卫星与网络, 2013 (5): 14- 14.

相似文献/References:

[1]杭观荣,康小录.电推进在深空探测主推进中的应用及发展趋势[J].火箭推进,2012,38(04):1.
　HANG Guan-rong,KANG Xiao-lu.Application and development trends of electric propulsion in deep-space primary propulsion[J].Journal of Rocket Propulsion,2012,38(02):1.
[2]张天平,刘乐柱,贾艳辉.电推进系统空心阴极产品试验技术[J].火箭推进,2010,36(01):54.
　Zhang Tianping,Liu Lezhu,Jia Yanhui.Test technology of hollow cathode products for electric propulsion system[J].Journal of Rocket Propulsion,2010,36(02):54.
[3]盛兆玄,冯玉军,徐卓,等.铁电阴极用于小功率电推力器[J].火箭推进,2008,34(02):37.
　Sheng Zhaoxuanl,Feng Yujun,Xu Zhuo,et al.Ferroelectric emission ：hodes for 1 OW lCcathod Ior low-power electric propulsion[J].Journal of Rocket Propulsion,2008,34(02):37.
[4]汪礼胜,唐德礼.阳极层推力器的研究现状与发展趋势[J].火箭推进,2006,32(01):24.
　Wang Lisheng,Tang Deli.The state of arts of thruster with anode layer[J].Journal of Rocket Propulsion,2006,32(02):24.
[5]杨乐,李自然,尹乐,等.脉冲等离子体推力器研究综述[J].火箭推进,2006,32(02):32.
　Yang Le,Li Ziran,Yin Le,et al.Review of pulsed plasma thruster[J].Journal of Rocket Propulsion,2006,32(02):32.
[6]潘海林,沈岩,魏延明,等.DFH-4卫星电推进系统的应用可行性研究[J].火箭推进,2006,32(05):22.
　Pan Hailin,Shen Yan,Wei Yanming,et al.Research on the application of electrical propulsion system on DFH-4 platform[J].Journal of Rocket Propulsion,2006,32(02):22.
[7]沈岩,魏延明,赵文华,等.低功率水电弧加热发动机的初步研究[J].火箭推进,2006,32(06):23.
　Shen Yan,Wei Yanming,Zhao Wenhua.Elementary research on low power arcjet with water propellant[J].Journal of Rocket Propulsion,2006,32(02):23.
[8]张郁.电推进技术的研究应用现状及其发展趋势[J].火箭推进,2005,31(02):27.
　Zhang Yu.Current status and trend of electric propulsion technology development and application[J].Journal of Rocket Propulsion,2005,31(02):27.
[9]顾左,郑茂繁,陈战东,等.氙离子火箭发动机的羽流及其污染分析[J].火箭推进,2004,(02):19.
[10]申连华,张星,陈艺,等.电推进工质的研究进展及发展趋势[J].火箭推进,2017,43(06):7.
　SHEN Lianhua,ZHANG Xing,CHEN Yi,et al.Research progress and development trend of working medium for electric propulsion[J].Journal of Rocket Propulsion,2017,43(02):7.

备注/Memo

收稿日期：2014-11-04；修回日期：2015-01-27 作者简介：左坤（1982—），男，硕士研究生，研究领域为空间全电推技术

更新日期/Last Update: 1900-01-01