[1] D Manzella,R Jankovsky,F Elliott,et al.Hall Thruster Plume Measurements On-Board the Russian Express Satellites[R].NASA/TM-2001-211217.
[2] N Sitnikova,D Volkov,I Maximov,et al.Hall Effect Thruster Interactions Data From the Russian Express-A2 and Express-A3 Satellites[R].NASA/CR-2003-212005.
[3] 张天平,唐福俊,田华兵,等.电推进航天器的特殊环境及其影响[J].航天器环境工程,2007,24(2): 88-94.
[4] 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(2):27-36.
[5] 田立成,龙建飞,郭宁,等.卫星敏感区域霍尔推力器束流沉积污染模型[J].真空科学与技术学报,2013,33(9): 883-887.
[6] Michael R Nakles,Lubos Brieda,Garrett D Reed.Experimental and Numerical Examination of the BHT-200 Hall Thruster Plume[R].AIAA 2007-5305.
[7] Smirnov A,Raitses Y,Fisch N J.Parametric Investigations of Miniaturized Cylindrical and Annular Hall Thrusters[C].Pasadena: 27th International Electric Propulsion Conference,2001.
[8] Daniel G.Courtney,Manuel Martinez-Sanchez.Diverging Cusped-Field Hall Thruster (DCHT)[C].Florence: The 30th Intenational Electric Propusion Conference,2007.
[9] Hofer P R,Randolph T M.Evaluation of a 4.5kW Commercial Hall Thruster System for NASA Science Missions[R].AIAA 2006-4469.
[10] Jerry L Ross,Alex Kieckhafer,Lyon B King.Performance Characteristics of a Low Isp Hall Thruster[R].AIAA 2006-4474.
[11] Jerry L.Ross.Probe Studies of a Hall Thruster at Low Voltages[D].Michigan: Michigan Technological University,2011.
[12] Richard R Hofer.High-Specific Impulse Operation of the BPT-4000 Hall Thruster for NASA Science Missions[R].AIAA 2010-6623.
[13] Manzella D,Jacobson D.Investigation of Low-Voltage/High-Thrust Hall Thruster Operation[R].AIAA 2003-5004.
[14] Hofer R R.Development and Characterization of High-Efficiency,High-Specific Impulse Xenon Hall Thrusters[D].Ann Arbor: University of Michigan,2004.
[15] Hofer R R,Gallimore A D.Efficiency Analysis of a High-Specific Impulse Hall Thruster[R].AIAA 2004-3602.
[16] Hofer R R,Gallimore A D.High-Specific Impulse Hall Thrusters,Part 2: Efficiency Analysis[J].Journal of Propulsion and Power,2006,22(4): 732-740.
[17] Brown D L.Investigation of Low Discharge Voltage Hall Thruster Characteristics and Evaluation of Loss Mechanisms[D].Ann Arbor: University of Michigan,2009.
[18] David Manzella,David Jacobson.Investigation of Low-Voltage/High-Thrust Hall Thruster Operation[R].AIAA 2003-5004.
[19] 康小录,江兆凌,汪南豪.稳态等离子体推力器低功率工作模式实验研究[J].推进技术,2001,22(4): 326-328.(KANG Xiao-Lu,WANG Zhao-ling,WANG Nan-hao.Experimental Investigation on Stationary Plasma Thruster (SPT) Operated at Lower Power Mode[J].Journal of Propulsion Technology,2001,22(4): 326-328.)(编辑:朱立影)收稿日期:2013-09-23;修订日期:2013-10-21。基金项目:重点实验室基金(9140C5504041001)。作者简介:田立成(1983—),男,硕士,工程师,研究领域为等离子体浸没离子注入材料改性研究、离子电推进和霍尔电推进等空间特种推进理论与实验技术研究、航天器充放电理论与实验技术研究等。E-mail:tlc1676@163.com
|