| Citation: | Characterization and measurement of doubly charged ions in xenon ion thruster beam[J]. Journal of Aerospace Power, 2017, 32(4): 970-975. doi: 10.13224/j.cnki.jasp.2017.04.024
|
| [1] |
Goebel D M，Katz I.Fundamentals of electric propulsion: ion and hall thrusters［M］.New York:John Wiley & Sons Inc,2008.
|
| [2] |
Brophy J R.The ion population system on NASA space technology 41 Champollion Comet Rendezvous Mission［R］.AIAA 99-2856，1999.
|
| [3] |
George J,Williams J R.Measurement of doubly charged ions in ion thruster plumes［R］.IEPC-01-310,2001.
|
| [4] |
Xie K,Martinez R A,Williams J D.Current-voltage characteristics of a cathodic plasma contactor with discharge chamber for application in electrodynamic tether propulsion［J］.Journal of Physics D:Applied Physics,2014,47(15):494-500.
|
| [5] |
Xie K,Xia Q,Williams J D,et al.Extracted current,bias voltage,and ion production of cathodic hollow-cathode-driven plasma contactors［J］.Journal of Spacecraft and Rockets,2015,52(4):1181-1192.
|
| [6] |
Peters R,Wilbur P J.Mercury ion thruster doubly charged ion model［R］.AIAA 76-1010,1976.
|
| [7] |
Peters R.Double ion production in mercury thrusters ［R］.NASA CR-135019,1976.
|
| [8] |
Goebel D M,Wirz R E,Katz I.Analytical ion thruster discharge performance model［R］.AIAA-2006-4486,2006.
|
| [9] |
刘畅,汤海滨,张振鹏,等.离子发动机加速栅极腐蚀深度的DFF测量与数值模拟［J］.航空动力学报,2008,23(3):574-579.LIU Chang,TANG Haibin,ZHANG Zhenpeng,et al.Numerical simulation and DFF measurement of ion thruster accelerator grid erosion depth［J］.Journal of Aerospace Power,2008,23(3):574-579.(in Chinese)
|
| [10] |
钟凌伟,刘宇,任军学,等.离子发动机栅极系统中束流离子的三维模拟［J］.航空动力学报,2010,25(9):2125-2131.ZHONG Lingwei,LIU Yu,REN Junxue,et al.Three-dimensional simulation of beam ions in ion thruster optics system［J］.Journal of Aerospace Power,2010,25(9):2125-2131.(in Chinese)
|
| [11] |
任军学,顾左,郭宁,等.离子发动机羽流特性的数值模拟［J］.航空动力学报,2013,28(6):1372-1379.REN Junxue,GU Zuo,GUO Ning,et al.Numerical simulation of characteristics of ion thruster plume［J］.Journal of Aerospace Power,2013,28(6):1372-1379.(in Chinese)
|
| [12] |
Nakano M.Doubly charged ion effect on life prediction accuracy of ion acceleration grid system［J］.Vacuum,2013,88(1)：70-74.
|
| [13] |
Sengupta A.Experimental and analytical investigation of a modified ring cusp NSTAR engine［R］.IEPC-2005-160,2005.
|
| [14] |
Wirz R E.Discharge plasma processes of ring-cusp ion thrusters［D］.Pasadena,California:California Institute of Technology,2005.
|
| [15] |
Poeschel R L,Beattie J R.Primary electric propulsion technology study［R］.NASA CR-159688,1979.
|
| [16] |
Foster J E,Patterson M J.Internal plasma properties and enhanced performance of an 8cm ion thruster discharge［R］.NASA TM 1999-209386,1999.
|
| [17] |
Farnell C C,Williams J D,Wilbur P J.Numerical simulation of ion thruster optics［R］.IEPC 03-0073,2003.
|
| [18] |
Boyd I,Crofton M.Computational study of extraction grid erosion through ion impact［R］.AIAA 2000-3664,2000.
|
| [19] |
Williams G J,Smith T B,Gallimore A D.30cm ion thruster discharge cathode erosion［R］.IEPC-2001-306,2001.
|
| [20] |
唐福俊,张天平.离子推力器羽流测量E×B探针设计及误差分析［J］.真空与低温,2007,13(2):77-80.TANG Fujun,ZHANG Tianping.Analysis and design of E×B probe for measurement of ion thruster plumes［J］.Vacuum and Cryogenics,2007,13(2):77-80.( in Chinese)
|
| [21] |
Brophy J R,Garner C E,Goodfellow K D.Electric propulsion system technology［R］.NASA CR-194100,1990.
|
| [22] |
Katz I,Gardner B M,Mandell M J,et al.Model of plasma contactor performance［J］.Journal of Spacecraft and Rockets,1997,34(6):824-828.
|
DownLoad: