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外加磁场对脉冲等离子体推力器性能的影响 被引量:2

Effects of Applied Magnetic Field on Performance of Pulsed Plasma Thruster
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摘要 为了研究外加磁场对PPT性能的影响,建立了PPT带外加磁场的机电模型,并用三种不同放电能量水平的PPT验证了该模型的可靠性。利用该模型研究了外加磁场强度、模式、位置以及长度对PPT性能的影响。结果表明,对于尾部馈送型PPT,当外加磁场增加时,PPT性能先增加后减小,存在最优的外加磁场强度。对于LES-6 PPT和LES-8/9 PPT,外加磁场从极板的最左端开始施加效果最好;当外加磁场强度分别为0.25T,0.50T,0.75T,1.00T时,这两种PPT对应的最适合施加磁场长度分别是1.3mm,1.8mm,2.1mm,2.3mm和1.6mm,2.8mm,3.4mm,3.7mm。对于TMU PPT,外加磁场从极板的最右端开始施加效果最好,但是施加磁场长度应该根据具体实验结果并结合仿真计算来决定。 In order to study the effects of applied magnetic field on the performance of PPT,an electromechanical model of PPT with an applied magnetic field was established,and the reliability of the model was verified by using three kinds of PPT with different discharge energy levels.Then,the effects of the intensity,mode,position and length of the applied magnetic field on the performance of PPT were studied by using the model.The results show that for the breech-fed PPT,the performance of PPT increases first and then decreases when the applied magnetic field increases,and the optimal applied magnetic field intensity exists.For LES-6 PPT and LES-8/9 PPT,the applied magnetic field was best applied from the far left end of the plate.When the applied magnetic field intensity was 0.25 T,0.50 T,0.75 T and 1.00 T,the optimum applied magnetic field lengths of these two PPT were 1.3 mm,1.8 mm,2.1 mm,2.3 mm and 1.6 mm,2.8 mm,3.4 mm,3.7 mm respectively.For TMU PPT,the applied magnetic field was best applied from the far right end of the plate,but the length of the applied magnetic field should be determined according to the experimental results and the simulation results.
作者 谭胜 吴建军 陈鑫 张宇 聂侥 李健 欧阳 TAN Sheng;WU Jian-jun;CHEN Xin;ZHANG Yu;NIE Yao', LI Jian;OU Yang(College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China;Aeronautics Engineering College,Air Force Engineering University,Xi'an 710038,China)
出处 《推进技术》 EI CAS CSCD 北大核心 2019年第5期1177-1188,共12页 Journal of Propulsion Technology
基金 国家自然科学基金面上项目(11772354)
关键词 机电模型 外加磁场 脉冲等离子体推力器 微小卫星 Electromechanical model Applied magnetic field Pulsed plasma thruster Microsatellite
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  • 1洪延姬,李修乾,窦志国.发展中的激光推进[J].推进技术,2009,30(4):490-494. 被引量:4
  • 2牛禄,王宏伟,杨威.用于微小卫星推进装置的脉冲等离子体推力器[J].上海航天,2004,21(5):39-43. 被引量:20
  • 3吴汉基,安世明.俄罗斯等离子体发动机的研究和应用[J].中国航天,1993(9):40-43. 被引量:5
  • 4林来兴.国外微小卫星在空间攻防中的应用研究[J].装备指挥技术学院学报,2006,17(6):47-49. 被引量:14
  • 5吴汉基.脉冲等离子体电火箭在卫星控制方面的应用[J].电工电能新技术,1986,(3):27-33.
  • 6Burton R L, Turchi P J. Pulsed plasma thruster [ J ]. Journal of Propulsion and Power, 1998, 14 (5): 716 - 735.
  • 7Mikellides Y G. Theoretical modeling and optimization of ablation-fed pulsed plasma thrusters [ D ]. USA : The Ohio State University, 1999.
  • 8Brito C M, Elaskar S A, Brito H H, et al. Zero-dimensional model for preliminary design of ablative pulsed plasma teflon thrusters [ J ]. Journal of Propulsion and Power, 2004, 20 (6) : 970 -977.
  • 9Laperriere D D. Electromechanical modeling and openloop control of parallel-plate pulsed plasma microthrusters with applied magnetic fields [ D ]. USA:Worcester Polytechnic Institute ,2005.
  • 10Keidar M, Boyd I D, Antonsen E L, et al. Optimization issues for a micropulsed plasma thruster [ J ]. Journal of Propulsion and Power, 2006, 22 ( 1 ) : 48 - 55.

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