20cm氙离子推力器性能扩展研究

推进技术 ›› 2015, Vol. 36 ›› Issue (7): 1116-1120.

• 电推进和其它推进 • 上一篇

20cm氙离子推力器性能扩展研究

郑茂繁,张天平,孟　伟,李兴坤,梁　凯

兰州空间技术物理研究所真空技术与物理国家级重点实验室，甘肃兰州 730000,兰州空间技术物理研究所真空技术与物理国家级重点实验室，甘肃兰州 730000,兰州空间技术物理研究所真空技术与物理国家级重点实验室，甘肃兰州 730000,兰州空间技术物理研究所真空技术与物理国家级重点实验室，甘肃兰州 730000,兰州空间技术物理研究所真空技术与物理国家级重点实验室，甘肃兰州 730000

发布日期:2021-08-15
作者简介:郑茂繁(1966—)，男，高级工程师，研究领域为电推进技术与工程。
基金资助:
真空低温技术与物理国家级重点实验室基金项目(9140C550206130C55003)。

Research of Improvement Performance for

National Key Laboratory of Science and Technology on Vacuum Technology and Physics，Lanzhou Institute of Physics，Lanzhou 730000，China,National Key Laboratory of Science and Technology on Vacuum Technology and Physics，Lanzhou Institute of Physics，Lanzhou 730000，China,National Key Laboratory of Science and Technology on Vacuum Technology and Physics，Lanzhou Institute of Physics，Lanzhou 730000，China,National Key Laboratory of Science and Technology on Vacuum Technology and Physics，Lanzhou Institute of Physics，Lanzhou 730000，China and National Key Laboratory of Science and Technology on Vacuum Technology and Physics，Lanzhou Institute of Physics，Lanzhou 730000，China

Published:2021-08-15

摘要/Abstract

摘要： 为了满足未来深空探测任务的需求，在20cm氙离子推力器的技术基础上，对其性能进行扩展提升研究，将推力提高50%，使推力由原来的40mN提高到60mN。通过对离子推力器工作参数的分析与研究，确定了离子推力器60mN推力模式的工作参数，并进行了优化实验。结果表明:性能扩展的20cm氙离子推力器推力提高到60mN，比冲提高到3500s，效率也提高到65%，并能够在40mN和60mN二种推力模式下工作。通过对2台推力器的组合，能够实现40，60，80，100，120mN五种推力工作模式。

关键词: 电推进；离子推力器；性能扩展；研究

Abstract: In order to meet the demand of deep space exploration，study was carried out based on the heritage of 20cm Xenon Ion Thruster to enhance its performance. Thrust increased from 40mN to 60mN，which is improved by 50%. The operating parameters at 60mN were finalized by the study and analysis and optimization with experiments. The results show that the thrust is extended to 60mN，and specific impulse increases to 3500s. Meanwhile efficiency is improved to 65%. After performance improvement，the thruster can be operated in 2 operating modes which are 40mN and 60mN，respectively. In addition，it is achievable for 40mN，60mN，80mN，100mN and 120mN 5 operating modes by combination of two thrusters，which can be adopted for deep space exploration.

Key words: Electric propulsion；Ion thruster；Improvement performance；Research

郑茂繁,张天平,孟　伟,李兴坤,梁　凯. 20cm氙离子推力器性能扩展研究[J]. 推进技术, 2015, 36(7): 1116-1120.

ZHENG Mao-fan,ZHANG Tian-ping,MENG Wei,LI Xing-kun,LIANG Kai. Research of Improvement Performance for[J]. Journal of Propulsion Technology, 2015, 36(7): 1116-1120.

参考文献

[1] Rawlin Vincent K, Sovey James S, John Hamley A. An Ion Propulsion System for NASA’s Deep Space Missions[R].AIAA 99-4612.
[2] Brophy John R, Marcucci Michael G, Ganapathi Cani B, et al. The Ion Propulsion System For Dawn[R].AIAA 2003-4542.
[3] Hitoshi Kuninaka, Yukio Shimizu, Tetsuya Yamada, et al. Report during Two Years on HAYABUSA Explorer Propelled by Microwave Discharge Ion Engines[R]. AIAA 2005-3673.
[4] Ahmed Rudwan Ismat M, Neil Wallace, Steve Clark. Twin Engine Tests of the T6 Ion Engine For ESA’s BepiColombo Mercury Mission[R].IEPC-2011-125.
[5] Anita Sengupta, Brophy John R, Goodfellow Keith D. Status of the Extended Life Test of the Deep Space1 Flight Spare Ion Engine After 30, 352 Hours of Operation [R]. AIAA 2003-4558.
[6] Greg Cardell1, Antonio Ulloa Severino, Michael Gross. The Design and Operation of the Dawn Power System [R]. AIAA 2012-3898.
[7] Zhangtianping. The LIPS-200 Ion Electric Propulsion System Development for the DFH-3B Satellite Platform[R]. IAC-13-C4.4.10, 2013.
[8] Dan M. Goebel and Ira Katz. Fundamentals of Electric Propulsion: Ion and Hall Thruster[M]. California:JPL Space Science and Technology Series, 2008: 24-28.
[9] 郑茂繁, 江豪成. 离子推进器性能评价方法[J].真空与低温, 2012, 18(4):223-227.
[10] 郑茂繁, 江豪成. 20cm氙离子推力器3000h寿命实验[J].航天器环境工程, 2009, 26(4):374-377.
[11] 刘金声. 离子束技术及应用 [M].北京:国防工业出版社, 1995.
[12] 郑茂繁, 江豪成. 离子推进器热特性测试与分析[J].真空与低温, 2011, 17(2):96-100.
[13] 郭宁, 唐福俊, 李文峰. 空间应用空心阴极研究进展[J]. 推进技术, 2012, 33(1): 155-160.(GUO Ning, TANG Fu-jun, LI Wen-feng. Advances in Spaceborne Hollow Cathode[J].Journal of Propulsion Technology, 2012, 33(1):155-160.)
[14] 贾艳辉, 郭宁, 李娟, 等. LIPS-200离子推力器关键部组件寿命分析[J].空间控制技术与应用, 2013, 39(4):54-58.
[15] 贾艳辉, 张天平, 李小平. 离子推力器加速栅寿命概率性分析[J]. 推进技术, 2011, 32(6): 766-769.(JIA Yan-hui, ZHANG Tian-ping, LI Xiao-ping. Probabilistic Evaluation of Ion Thruster Accelerator Grid Life[J].Journal of Propulsion Technology, 2011, 32(6):766-769.)(编辑:张荣莉)　　　　　　　　　　　　　*　收稿日期:2014-05-26；修订日期:2014-07-17。基金项目:真空低温技术与物理国家级重点实验室基金项目(9140C550206130C55003)。作者简介:郑茂繁(1966—),男,高级工程师,研究领域为电推进技术与工程。E-mail:zhengmaofan@hotmail.com

20cm氙离子推力器性能扩展研究

Research of Improvement Performance for

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 0

编辑推荐

Metrics

本文评价