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全电推进GEO卫星平台发展研究 被引量:20

Development Approach to All-electric Propulsion GEO Satellite Platform
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摘要 介绍了国外电推进系统在地球静止轨道(GEO)卫星上的应用阶段,以及包括波音卫星系统-702SP(BSS-702SP)在内的主要全电推进卫星平台;总结了全电推进卫星平台在商业市场竞争、平台技术创新、中型通信卫星市场需求方面的发展动因;提炼了全电推进卫星平台涉及的大推力、高比冲、双模式电推进系统,以及全轨道、小推力、自主变轨和位置保持等关键技术;提出了我国全电推进卫星平台开发的目标及发展途径。 The development stage of electric propulsion system and the main all-electric propulsion GEO satellite platforms including BSS-702SP are introduced. The development motivations of all- electric propulsion satellite platform are summarized including the commercial market competi- tion, platform technical innovation, and market demand for medium-sized telecommunication satellites. The key technologies of all-electric propulsion satellite platform are refined such as high thrust, high impulse, dual mode electric propulsion system, the whole orbit and low-thrust autonomous orbit maneuver, and position keeping. Finally, the paper proposes the development target and the approach of China's all-electric propulsion platform.
作者 周志成 高军
出处 《航天器工程》 北大核心 2015年第2期1-6,共6页 Spacecraft Engineering
关键词 通信卫星平台 全电推进系统 小推力变轨 telecommunication satellite platform all-electric propulsion system low-thrust orbit maneuver
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参考文献10

  • 1Defense Industry Daily.Next-stage C4ISR bandwidth:the AEHF satellite program[EB/OL].[2014-12-20].https://www.defenseindustrydaily.com/nextstagec4isr-bandwidth-the-us-militarys-aehf-program-updated-02165/.
  • 2Steven A Feuerborn1,David A Neary,Julie M Perkins.Finding a way:Boeing’s“All electric propulsion satellite”[C]//Proceedings of the 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.Washington D.C.:AIAA,2013:1-5.
  • 3H Lübberstedt,A Schneider,H Schuff,et al.Development of the European small geostationary satellite SGEO[C]//Proceedings of the IAA Symposium on Small Satellite Systems and Services(4S).Stockholm:IAA,2008.
  • 4周志成,王敏,李烽,蔡国飙,汤海滨.我国通信卫星电推进技术的工程应用[J].国际太空,2013(6):40-45. 被引量:11
  • 5张天平,田华兵,陈娟娟.LIPS-200离子推力器寿命地面试验方案研究[J].航天器工程,2012,21(4):111-116. 被引量:5
  • 6张志远,田杨,王平阳,吴建军.霍尔推力器寿命实验和计算分析[J].火箭推进,2014,40(3):16-22. 被引量:2
  • 7孙明明,张天平,王亮.30cm口径离子推力器热特性模拟分析[J].真空与低温,2014,20(3):158-162. 被引量:9
  • 8By Zhong Xiaoqing.Electric Propulsion DFH-3B Communications Satellite Platform[J].Aerospace China,2013,14(4):17-18. 被引量:2
  • 9Ronald L Corey,Nicolas Gascon,Jorge J Delgado,et al.Performance and evolution of stationary plasma[C]//Proceedings of the 28th AIAA International Communications Satellite Systems Conference(ICSSC-2010).Washington D.C.:AIAA,2010:1-20.
  • 10M Konstantinov.The analysis of influence of electrical propulsion characteristics on efficiency of transport maneuvers[C/OL].[2014-12-20].http://erps.spacegrant.org/uploads/images/images/iepc_articledownload_1988-2007/2007index/IEPC-2007-212.pdf.

二级参考文献20

  • 1张天平.国外离子和霍尔电推进技术最新进展[J].真空与低温,2006,12(4):187-193. 被引量:61
  • 2Dankanich J W. Lifetime qualification standard for electric thrusters,AIAA 2009-5095[R].Washington:AIAA,2009.
  • 3Chien K R,Hart S,Tighe W G. L-3 communications ETI electric propulsion overview,IEPC 2005-075[A].Washington:AIAA,2005.
  • 4Tighe W G,Chien K-R,Spears R. Ion thruster development at L 3 ETI for small satellite applications,IEPC 07 024[A].Washington:AIAA,2007.
  • 5Tighe W G,Chien K-R,Solis Z. The 25 cm XIPS(c) life test and post-test analysis,IEPC 2009-161[A].Washington:AIAA,2009.
  • 6Killinger R,Bassner H,Kukies R. Results of the 15000 hours lifetime test for the RITA ion propulsion on ESA''''s ARTEMIS satellite,IEPC 2001082[A].Washington:AIAA,2001.
  • 7Killinger R,Bassner H,Leiter H. RITA ion propulsion for ARTEMIS results close to the completion of the life test,AIAA 2001-3490[R].Washington:AIAA,2001.
  • 8Killinger R,Leiter H,Kukies R. RITA ion propulsion systems for commercial and scientific applications,AIAA 2007 5200[R].Washington:AIAA,2007.
  • 9Shimada S,Nishida E,Noro T. Ion thruster endurance test using development model thruster for ETS-Ⅵ, IEPC1993-169[A].Washington:AIAA,1993.
  • 10Ozaki T,Nishida E,Gotoh Y. Development status of 20mN xenon ion thruster,AIAA 2000-3277[R].Washington:AIAA,2000.

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