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马隆飞, 贺建武, 罗军, 章楚, 杨超, 付佳豪, 段俐, 康琦. 射频离子推力器研究进展[J]. 深空探测学报(中英文), 2024, 11(2): 111-123. DOI: 10.15982/j.issn.2096-9287.2024.20230036
引用本文: 马隆飞, 贺建武, 罗军, 章楚, 杨超, 付佳豪, 段俐, 康琦. 射频离子推力器研究进展[J]. 深空探测学报(中英文), 2024, 11(2): 111-123. DOI: 10.15982/j.issn.2096-9287.2024.20230036
MA Longfei, HE Jianwu, LUO Jun, ZHANG Chu, YANG Chao, FU Jiahao, DUAN Li, KANG Qi. Research Progress of Radio Frequency Ion Thruster[J]. Journal of Deep Space Exploration, 2024, 11(2): 111-123. DOI: 10.15982/j.issn.2096-9287.2024.20230036
Citation: MA Longfei, HE Jianwu, LUO Jun, ZHANG Chu, YANG Chao, FU Jiahao, DUAN Li, KANG Qi. Research Progress of Radio Frequency Ion Thruster[J]. Journal of Deep Space Exploration, 2024, 11(2): 111-123. DOI: 10.15982/j.issn.2096-9287.2024.20230036

射频离子推力器研究进展

Research Progress of Radio Frequency Ion Thruster

  • 摘要: 详细介绍了射频离子推力器的工作原理,以及近60年微牛级和毫牛级射频离子推力器的研究历程和成果。射频离子推进系统涉及多项关键技术难题,针对工质选取、射频电路阻抗匹配、气体流量控制、电中和控制和寿命问题提出了初步解决方案,结合射频离子推力器未来应用的需求,展望了射频离子推力器的发展趋势和研究方向。

     

    Abstract: The principle of radio frequency ion thrusters(RIT), as well as the research history and achievements of micro-newton and milli-Newton RIT at home and abroad in the past 60 years, was explained in detail. The radio frequency ion propulsion system involves a number of key technical challenges. Preliminary solutions to the problems of propellant selection, radio frequency(RF)circuit impedance matching, gas flow control, electrical neutralization control and lifetime were proposed, and the development trend and research direction were put forward combined with the future application of RIT.

     

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