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作 者:Yuxuan ZHONG Yu ZHANG Jianjun WU Peng ZHENG
出 处:《Chinese Journal of Aeronautics》2024年第10期172-183,共12页中国航空学报(英文版)
基 金:funded by the National Natural Science Foundation of China (No. T2221002);the Hunan Provincial Natural Science Foundation, China (No. 2024JJ5405)
摘 要:Plasma discharge stability is an important problem in atmosphere-breathing electric propulsion system when maintaining long-term missions at ultra-low earth orbit.This paper designed an inductively coupled plasma source to imitate the ionization section.The effect of inflow rate and Radio Frequency(RF)power on the plasma discharge mode transition is experimentally studied.A discharge mode detection method is proposed,which determines the discharge mode by identifying the morphology of the plasma core.By using the method,the discharge mode transition is quantified and a control model based on the parameter sensitivity is constructed.To verify the method,the spectra are measured and the electron temperature spatial distribution is calculated.And the method has been proven effective.The results show that the inductively coupled discharge contains capacitive components affected by the mass flow rate and the radio frequency power.The plasma characteristics can be maintained stably by controlling the radio frequency power when the mass flow rate randomly changes in a certain range.It is demonstrated that the application of detection method effectively identifies the discharge mode,which is a promising active control method for the plasma discharge mode.
关 键 词:Atmosphere-breathing electric propulsion Inductively coupled plasma Discharge mode transition Optical diagnosis Ultra-low earth orbit
分 类 号:V439.4[航空宇航科学与技术—航空宇航推进理论与工程]
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