ECRIT Ion Source Performance Analysis based on Geobel Model
-
摘要: 利用Geobel模型对电子回旋共振离子推力器的离子源性能进行了计算,分析工质利用率与放电损耗的关系、电子温度与离子源性能的关系、离子源长度和栅极有效透明度对放电损耗和工质利用率的影响。采用Geobel模型对电子回旋共振离子推力器性能的计算结果为:20 cm ECRIT离子源在100 mm轴向长度、80%栅极有效透明度条件下,工质利用率为90%,放电损失为203 W/A;10 cm ECRIT离子源在40 mm轴向长度、80%栅极有效透明度条件下,工质利用率为86%,放电损失为300 W/A。结果表明:采用Geobel模型算法计算结果与国外文献数据的相对误差小于5%,利用该模型对电子回旋共振离子推力器离子源性能分析的方法有效、合理。Abstract: This paper uses the Geobel model to study the plasma performance of the ion source of an electron cyclotron resonance ion thruster. It analyzes the relationship between mass utilization efficiency and discharge loss, electron temperature and ion source performance, influence of ion source length and grid effective transparency on the discharge loss and mass utilization efficiency. The calculation results of the ion source performance show that the mass utilization efficiency and the discharge loss are 90% and 203 W/A respectively for 20 cm ECRIT ion source with 100 mm axial length and the 80% grid effective transparency; the mass utilization efficiency and discharge loss are 86% and 300 W/A respectively for 10 cm ECRIT ion source with 40 mm axial length and the 80% grid effective transparency. The performance analysis demonstrates that the ion source performance data calculated with the Geobel model has a relative error of less than 5% compared with the data published in the open literature.
-
[1] Tsukizaki R, Koizumi H, Nishiyama K, et al. Measurement of axial neutral density profiles in a microwave discharge ion thruster by laser absorption spectroscopy with optical fiber probes[J]. Review of Scientific Instruments, 2011,82(12):123103 [2] Kuninaka H, Nishiyama K, Shimizu Y, et al. Flight status of cathode-Less microwave discharge ion engines onboard HAYABUSA asteroid explorer[C]//40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 11-14, 2004, Fort Lauderdale, Florida. Florida:AIAA, 2004 [3] 杨涓,石峰,杨铁链,等.电子回旋共振离子推力器放电室等离子体数值模拟[J].物理学报,2010,59(12):8701-8706 Yang J, Shi F, Yang T L, et al. Numerical simulation on the plasma field within discharge chamber of electron cyclotron resonance ion thruster[J]. Acta Physica Sinica, 2010,59(12):8701-8706(in Chinese) [4] 杨涓,王阳,孟志强,等.电子回旋共振离子推力器放电室等离子体静电探针诊断[J].机械科学与技术,2013,32(2):203-208 Yang J, Wang Y, Meng Z Q, et al. Electrostatic probe diagnosis on the plasma in the discharge chamber of an electron cyclotron resonance ion thruster[J]. Mechanical Science and Technology for Aerospace Engineering, 2013,32(2):203-208(in Chinese) [5] 杨涓,冯冰冰,罗立涛,等.氩气和氪气作为ECR中和器工质的性能比较[J].高电压技术,2015,41(9):2850-2855 Yang J, Feng B B, Luo L T, et al. Performance comparison between ECR neutralizers using argon and krypton propellant[J]. High Voltage Engineering, 2015,41(9):2850-2855(in Chinese) [6] 汤明杰,杨涓,金逸舟,等.微型电子回旋共振离子推力器离子源结构优化实验研究[J].物理学报,2015,64(21):215202 Tang M J, Yang J, Jin Y Z, et al. Experimental optimization in ion source configuration of a miniature electron cyclotron resonance ion thruster[J]. Acta Physica Sinica, 2015,64(21):215202(in Chinese) [7] 汤明杰,杨涓,冯冰冰,等.微推力ECR离子推力器等离子体源电子获能计算分析[J].推进技术,2015,36(11):1741-1747 Tang M J, Yang J, Feng B B, et al. Calculation analysis on electron heating within plasma source used by micro ECR ion thruster[J]. Journal of Propulsion Technology, 2015,36(11):1741-1747(in Chinese) [8] 梁雪,杨涓,王雲民.电子回旋共振中和器内静磁场及微波电磁场的数值计算[J].推进技术,2014,35(2):276-281 Liang X, Yang J, Wang Y M. Numerical computation of static magnetic and microwave electromagnetic fields in electron cyclotron resonance neutralizer[J]. Journal of Propulsion Technology, 2014,35(2):276-281(in Chinese) [9] 陈茂林,毛根旺,夏广庆,等.电子回旋共振离子推力器栅极光学系统的PIC/MCC模拟[J].推进技术,2012,33(1):150-154 Chen M L, Mao G W, Xia G Q, et al. PIC/MCC Simulation on the optical of electron cyclotron resonance ion thruster[J]. Journal of Propulsion Technology, 2012,33(1):150-154(in Chinese) [10] Brophy J R, Wilbur P J. Simple performance model for ring and line cusp ion thrusters[J]. AIAA Journal, 1985,23(11):1731-1736 [11] Goebel D M, Wirz R E, Katz I. Analytical ion thruster discharge performance model[J]. Journal of Propulsion and Power, 2007,23(5):1055-1067 [12] 利力伯曼,里登伯格.等离子体放电原理与材料处理[M].蒲以康,译.北京:科学出版社,2007 Lieberman M A, Lichtenberg A J. Principles of plasma discharges and materials processing[M]. Pu Y K, trans. Beijing:Science Press, 2007(in Chinese) [13] Szabo J J Jr. Fully kinetic numerical modeling of a plasma thruster[D]. Cambridge:Massachusetts Institute of Technology, 2001 [14] Jin Y Z, Yang J, Tang M J, et al. Diagnosing the fine structure of electron energy within the ECRIT ion source[J]. Plasma Science and Technology, 2016,18(7):744-750 [15] 于达仁,刘辉,丁永杰,等.空间电推进原理[M].哈尔滨:哈尔滨工业大学出版社,2014 Yu D R, Liu H, Yu Y J, et al. Fundamentals of space electric propulsion[M]. Harbin:Harbin Institute of Technology Press, 2014(in Chinese)
点击查看大图
计量
- 文章访问数: 126
- HTML全文浏览量: 25
- PDF下载量: 6
- 被引次数: 0