[1] 孙明明, 张天平, 王亮, 等. 30cm口径离子推力器栅极组件热应力及热形变计算模拟[J]. 推进技术, 2016, 37(7): 1393-1400. (SUN Ming-ming, ZHANG Tian-ping, WANG Liang, et al. Thermal Stress and Thermal Deformation Analysis of Grids Assembly for 30cm Diameter Ion Thruster[J]. Journal of Propulsion Technology, 2016, 37(7): 1393-1400.)
[2] Lichtin D. An Overview of Electric Propulsion Activities in US Industry[R]. AIAA 2005-3532.
[3] Chien K R, Tighe W, Bond T, et al. An Overview of Electric Propulsion at L-3 Communications Electron Technologies Inc[R]. AIAA 2006-4322.
[4] Sengupta A, Brophy J, Anderson J, et al. An Overview of the Results from the 30000Hr Life Test of Deep Space 1 Flight Spare Ion Engine[R]. AIAA 2004-3608.
[5] Noord J. Lifetime Assessment of the NEXT Ion Thruster[R]. AIAA 2007-5274.
[6] Hayashi M. Determination of Electron-Xenon Total Excitation Cross-Section[J]. Journal of Physics D: Applied Physics, 1983, 16(1): 581–589.
[7] Bond, Latham. Ion Thruster Extraction Grid Design and Erosion Modeling Using Computer Simulation[R]. AIAA 1995-2923.
[8] Rapp D, Francis. Charge Exchange Between Gaseous Ions and Atoms[J]. Journal of Chemical Physics, 1962, 37(11): 2631-2645.
[9] Beattie J, Matossian J. High Power Xenon Ion Thruster[R]. AIAA 90-2540.
[10] Goebel D, Jameson K, Watkins R, et al. Cathode and Keeper Plasma Measurements Using an Ultra-Fast Miniature Scanning Probe[R]. AIAA 2004-3430.
[11] Mikellides I, Katz I, Mandell M. A 1-D Model of The Hall-Effect Thruster with an Exhaust Region[R]. AIAA 2001-3505.
[12] Haag T, Soulas G. Performance of 8cm Pyrolytic-Graphite Ion Thruster Optics[R]. AIAA 2002-4335.
[13] Soula G, Frandina M. Ion Engine Grid Gap Measurement[R]. AIAA 2004-3961.
[14] Wells A, Harrison M. Experimental Studies of Ion Extraction Ion Loss and Energy Balance in a SERT II Type Ion Thruster[R]. AIAA 1970-1091.
[15] Miller J, Pullins S, Levandier D, et al. Xenon Charge Cross Section for Electrostatic Thruster Models[J]. Journal of Applied Physics, 2002, 91(3): 984-991.
[16] Katz I, Anderson J, Polk J, et al. One Dimensional Hollow Cathode Model[J]. Journal of Propulsion and Power, 2003, 19(4): 595–600.
[17] Rapp D, Englander P. Total Cross Section for Ionization and Attachment in Gases by Electron Impact I positive Ionization[J]. The Journal of Chemical Physics, 1965, 43(5): 1464-1479.
[18] 孙明明, 张天平, 陈娟娟, 等. LIPS-200环形会切磁场离子推力器热模型计算分析[J]. 推进技术, 2015, 36(8): 1274-1280. (SUN Ming-ming, ZHANG Tian-ping, CHEN Juan-juan, et al. Thermal Model of LIPS-200 Ring-Cusp Magnet Field Ion Thruster[J]. Journal of Propulsion Technology, 2015, 36(8): 1274-1280.)
[19] Brophy J, Katz I, Polk J, et al. Numerical Simulation of Ion Thruster Accelerator Grid Erosion[R]. AIAA 2002-4261.
[20] Beattie J. A Model for Predicting the Wearout Lifetime of the LeRC/Hughes 30cm Mercury Ion Thruster[R]. AIAA 79-2079.
[21] Tartz M, Neumann H. Validated Ion Thruster Grid lifetime Simulation[R]. AIAA 2006-5001.
[22] Noord J, Herman D. Application of the NEXT Ion Thruster Lifetime Assessment to Thruster Throttling[R].AIAA 2008-4526.
[23] Funaki I, Makano M, Kajimura Y, et al. A Numerical Tool for Lifetime Evaluation of Ion Thruster’s Ion Optics[R]. AIAA 2011-5734. 收稿日期:2018-03-14;修订日期:2018-05-09。基金项目:真空低温技术与物理重点实验室基金(6142207030103)。作者简介:孙明明,博士,高级工程师,研究领域为空间电推进技术。E-mail: smmhappy@163.com通讯作者:陈小强,博士,教授,研究领域为计算电磁学。E-mail: 13919289637@139.com(编辑:梅瑛)
|