[1] 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(5): 385-392. (WU Han-ji, JIANG Yuan-da, ZHANG Zhi-yuan. Application and Development Trend of Electric Propulsion Technology[J]. Journal of Propulsion Technology, 2003, 24(5): 385-392.)
[2] 郭宁, 唐福俊, 李文峰. 空间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.)
[3] 丁永杰, 扈延林, 颜世林, 等. 聚焦磁场及发散磁场对霍尔推力器壁面侵蚀的影响研究[J]. 推进技术, 2015, 36(5): 795-800. (DING Yong-jie, HU Yan-lin, YAN Shi-lin. Effects of Focusing and Diverging Magnetic Field Topology on Hall Thruster Channel Wall Erosion[J]. Journal of Propulsion Technology, 2015, 36(5): 795-800.)
[4] 宁中喜. 霍尔推力器羽流发散角的定向探针测量方法[J]. 推进技术, 2011, 32(6): 895-899. (NING Zhong-xi. Hall Thruster Plume Divergence Angle Directional Probe Measurement Method[J]. Journal of Propulsion Technology, 2011, 32(6): 895-899.)
[5] 温正, 王敏, 仲小清. 多任务模式电推进技术[J]. 航天器工程, 2014, 23(1): 118-123.
[6] 郭宁, 江豪成, 高军, 等. 离子发动机空心阴极失效形式分析[J]. 真空与低温, 2005 , 11(4): 239-242.
[7] Daniel A Herman, Luis R Pi?ero, James S Sovey. NASA’s Evolutionary Xenon Thruster (NEXT) Component Verification Testing[R]. ASME CT 2008-4812.
[8] 张岩, 康小录, 乔彩霞. 六硼化镧与钡钨空心阴极的放电特性实验研究[J]. 真空电子技术, 2013(3): 12-20.
[9] 张天平, 唐福俊, 田华兵. 国外电推进系统空心阴极技术[J]. 上海航天, 2008(1): 39-46.
[10] 郭宁, 邱家稳, 顾佐, 等. 20cm 氙离子发动机空心阴极 3000h 寿命试验[J]. 真空与低温, 2006, 12(4): 204-206.
[11] Makela J M, Massey D R, King L B. Bismuth Hollow Cathode for Hall Thrusters[J]. Journal of Propulsion and Power, 2008, 24(1): 142-146.
[12] Anita Sengupta. Destructive Physical Analysis of Hollow Cathodes from the Deep Space 1 Flight Spare Ion Engine 30000 Hour Life Test[C]. Princeton University: 29th International Electric Propulsion Conference, 2005.
[13] William G Tighe, Ken Freick, Kuei-Ru Chien. Performance Evaluation and Life Test of the XIPS Hollow Cathode Heater[R]. AIAA 2005-4066.
[14] Dan M Goebel, Ronald M Watkins. Compact Lanthanum Hexaboride Hollow Cathode[J]. Review of Science Instruments, 2010, 81(8): 083504.
[15] Dan M Goebel, James E Polk. Lanthanum Hexaboride Hollow Cathode for the Asteroid Redirect Robotic Mission 12.5kW Hall Thruster[C]. Hyogo-Kobe Japan: 34th International Electric Propulsion Conference, 2015.
[16] 杨威, 陈继巍, 贾艳辉, 等. 离子推力器空心阴极点火可靠性评价研究[J]. 真空与低温, 2015, 21(4):96-102.
[17] 乔彩霞, 张岩, 康小录, 等. 80mN霍尔推力器空心阴极寿命试验[J]. 火箭推进, 2014, (40)4: 11-15.
[18] Timothy R. Sarver-Verhey. 28000 Hour Xenon Hollow Cathode Life Test Results[C]. Cleveland, Ohio: 25th International Electric Propulsion Conference, 1997.(编辑:史亚红) * 收稿日期:2016-05-17;修订日期:2016-06-29。基金项目:国家自然科学基金(U1332135)。作者简介:李文博,男,博士生,研究领域为等离子体推进。 E-mail: liwenbO201120@163.com
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