Research on Parameter Design Method of Concentric Nested Hall Thruster
-
摘要:
结合未来国内外对大功率场霍尔推力器的需求，论述同心嵌套通道式霍尔推力器研究现状，技术优势。针对嵌套通道式霍尔推力器参数设计方法的空白，介绍了一种可行的嵌套通道式霍尔推力器的结构和磁路；提出了一种以阳极功率和比冲为输入，确定嵌套通道式霍尔推力器通道数目、各通道结构参数和工作参数的方法；结合磁路设计和热设计，给出了优化嵌套通道式霍尔推力器的参数的路径；填补嵌套通道式霍尔推力器参数设计和优化的空白，为其工程应用提供参考。
-
关键词:
- 嵌套通道式霍尔推力器/
- 参数设计/
- 磁路设计
Abstract:According to the future demand for high power Hall thruster at home and abroad， the research status and technical advantages of concentric nested channel Hall thrusters are discussed. The structure and magnetic circuit of a feasible nested channel Hall thruster are introduced. A method is proposed to determine the structure of the Hall thruster. The method of optimizing the parameters of the nested Hall thruster is given. The process of the nested channel is expected to be filled with the channel design and the thermal design. It will provide reference for engineering application in the future.
-
[1] 杨福全,赵以德,李娟,等. 主带小行星采样返回任务中的离子电推进应用方案[J].深空探测学报,2015,2(2):168-173. Yang F Q,Zhao Y D,Li J,et al. Application scheme of ion electric propulsion system for main-belt asteroid sample and return mission[J]. Journal of Deep Space Exploration,2015,2(2):168-173. [2] 郑茂繁,耿海,梁凯,等. 用于小行星探测的离子推力器技术研究[J]. 深空探测学报,2015,2(3):236-240. Zheng M F,Geng H,Liang K,et al. Research on ion thruster technology for asteroid exploration[J]. Journal of Deep Space Exploration,2015,2(3):236-240. [3] Koppel C R,Marchandise F,Prioul M,et al. The SMART-1 electric propulsion subsystem around the Moon:in flight experience[C]//proceedings of 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference. Tucson:AIAA,2005. [4] Brophy J R,Gershman R,Strange N,et al. 300 kW Solar electric propulsion system configuration:ion for human exploration of near-Earth asteroids[C]//47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. San Diego,California:AIAA. [5] Manzella D,Hack K. High-power Solar electric propulsion for future NASA missions[C]//50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. Cleveland:AIAA,2014. [6] Bérend N, Cliquet E, Ruault J M, et al. How fast can we go to Mars using high power electric propulsion[C]//48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Atlanta,Georgia:AIAA,2012. [7] 杭观荣,康小录. 国外大功率等离子体推力器研究概况及对我国的发展建议[C]//第九届中国电推进技术学术研讨会.北京:中国宇航学会,2013. Hang G R,Kang X L. The research of high power plasma thrusters abroad and the development suggestions for our country[C]//The Ninth China Electric Propulsion Technology Symposium. Beijing:Chinese Society of Astronautics,2013. [8] 张天平,陈娟娟,李兴坤. 中高功率离子推力器的性能参数分析研究[J].真空与低温,2012,18(1):9-20. Zhang T P,Chen J J,Li X K. Performance parameter analysis of the moderate and higher power ion thruster[J]. Vacuum and Cryogenics,2012,18(1):9-20. [9] 吴汉基,蒋远大,张志远. 电推进技术的应用与发展趋势[J]. 推进技术,2003,24(05):385-392. Wu H J,Jiang Y D,Zhang Z Y. Application and development trend of electric propulsion technology[J]. Journal of Propulsion Technology,2003,24(05):385-392. [10] Liang R. The combination of two concentric discharge channels into a nested Hall-effect thruster[D]. Michigan:The University of Michigan,2013. [11] Florenz R E. The X3100-kW class nested-channel Hall thruster:motivation,implementation and initial performance[D]. Michigan:The University of Michigan,2014. [12] Shagayda A. On scaling of Hall effect thrusters[J]. Plasma Science,IEEE Transactions,2015,43(1):12-28. [13] Shagayda A A,Gorshkov O A. Hall-thruster scaling laws[J]. Journal of Propulsion and Power,2013,29(2):466-474. [14] Morozov A I,Savelyev V V. Fundamentals of stationary plasma thruster theory[M] Germany:Springer US,2000. [15] Manzella D. Scaling Hall thrusters to high power[D]. USA:Stanford University,2005. -
点击查看大图
计量
- 文章访问数:2403
- HTML全文浏览量:43
- PDF下载量:980
- 被引次数:0
下载:
