胡竟, 江豪成, 王亮, 等. 阴极挡板对30 cm氙离子推力器性能影响的研究[J]. 真空与低温, 2015, 21(2): 103-106. DOI: 10.3969/j.issn.1006-7086.2015.02.010
引用本文: 胡竟, 江豪成, 王亮, 等. 阴极挡板对30 cm氙离子推力器性能影响的研究[J]. 真空与低温, 2015, 21(2): 103-106. DOI: 10.3969/j.issn.1006-7086.2015.02.010
HU Jing, JIANG Haocheng, WANG Liang, et al. STUDY ON PERFORMANCES OF 30 cm XENON ION THRUSTER SUBJECTED TO CATHODE BAFFLE[J]. VACUUM AND CRYOGENICS, 2015, 21(2): 103-106. DOI: 10.3969/j.issn.1006-7086.2015.02.010
Citation: HU Jing, JIANG Haocheng, WANG Liang, et al. STUDY ON PERFORMANCES OF 30 cm XENON ION THRUSTER SUBJECTED TO CATHODE BAFFLE[J]. VACUUM AND CRYOGENICS, 2015, 21(2): 103-106. DOI: 10.3969/j.issn.1006-7086.2015.02.010

阴极挡板对30 cm氙离子推力器性能影响的研究

STUDY ON PERFORMANCES OF 30 cm XENON ION THRUSTER SUBJECTED TO CATHODE BAFFLE

  • 摘要: 束流分布是表征离子推力器性能的关键技术指标,直接影响到离子推力器的工作稳定性和可靠性。针对引出束流分布不均匀导致30 cm氙离子推力器离子光学系统打火保护的问题,开展了阴极挡板性能试验,研究分析了阴极挡板对离子光学系统引出束流的影响作用关系,以及设置阴极挡板前后和设置不同规格阴极挡板时推力器放电室性能变化规律。试验表明:设置阴极挡板可有效提高离子光学系统引出束流分布的均匀性,进而改善推力器的连续工作稳定性;同时,设置阴极挡板后,推力器在高功率工作模式下的放电室阳极电压、放电损耗与未设置阴极挡板相比有明显增大,且放电室阳极电压、放电损耗随阴极挡板直径的增大而增大。研究为提高30 cm氙离子推力器工作稳定性提供技术指导。

     

    Abstract: Beam distribution is an important technical parameter to indicate the performance of ion thruster,it directly influences the working stability and reliability of ion thruster.Aiming at the problem of spark down of the ion optics system for 30 cm Xenon ion thruster because of the beam distribution imbalance,the cathode baffle test was developed and the relationship between the cathode baffle and the beam distributions was observed.The influence of fore-and-back setting cathode baffle and setting different types cathode baffle on the discharge chamber performance were researched.The results showed that setting cathode baffle could effectively improve beam distributions of the ion optics system,and the working stability of the ion thruster.The anode voltage and discharge loss was enhanced after setting cathode baffle in the high power mode,and with the diameter of the cathode baffle's increasing.Above research will certainly provide technical guidance for improving working stability for the 30 cm Xenon ion thruster.

     

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