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Effects of Three Typical Resistivity Models on Pulsed Inductive Plasma Acceleration Modeling 被引量:2
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作者 孙新锋 贾艳辉 +6 位作者 张天平 吴宸辰 温晓东 郭宁 金海 柯于俊 郭伟龙 《Chinese Physics Letters》 SCIE CAS CSCD 2017年第12期46-50,共5页
The effects of three different typical resistivity models(Spitzer, Z&L and M&G) on the performance of pulsed inductive acceleration plasma are studied. Numerical results show that their influences decrease with th... The effects of three different typical resistivity models(Spitzer, Z&L and M&G) on the performance of pulsed inductive acceleration plasma are studied. Numerical results show that their influences decrease with the increase of the plasma temperature. The significant discriminations among them appear at the plasma temperature lower than 2.5 eV, and the maximum gap of the pulsed inductive plasma accelerated efficiency is approximately 2.5%.Moreover, the pulsed inductive plasma accelerated efficiency is absolutely related to the dynamic impedance parameters, such as voltage, inductance, capacitance and flow rate. However, the distribution of the efficiency as a function of plasma temperature with three resistivity models has nothing to do with the dynamic impedance parameter. 展开更多
关键词 In Effects of Three Typical Resistivity Models on pulsed inductive plasma Acceleration Modeling
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Spatio-temporal measurements of overshoot phenomenon in pulsed inductively coupled discharge
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作者 Xiang-Yun Lv Fei Gao +1 位作者 Quan-Zhi Zhang You-Nian Wang 《Chinese Physics B》 SCIE EI CAS CSCD 2021年第4期369-375,共7页
Pulse inductively coupled plasma has been widely used in the microelectronics industry,but the existence of overshoot phenomenon may affect the uniformity of plasma and generate high-energy ions,which could damage the... Pulse inductively coupled plasma has been widely used in the microelectronics industry,but the existence of overshoot phenomenon may affect the uniformity of plasma and generate high-energy ions,which could damage the chip.The overshoot phenomenon at various spatial locations in pulsed inductively coupled Ar and Ar/CF_(4) discharges is studied in this work.The electron density,effective electron temperature,relative light intensity,and electron energy probability function(EEPF) are measured by using a time-resolved Langmuir probe and an optical probe,as a function of axial and radial locations.At the initial stage of pulse,both electron density and relative light intensity exhibit overshoot phenomenon,i.e.,they first increase to a peak value and then decrease to a convergent value.The overshoot phenomenon gradually decays,when the probe moves away from the coils.Meanwhile,a delay appears in the variation of the electron densities,and the effective electron temperature decreases,which may be related to the reduced strength of electric field at a distance,and the consequent fewer high-energy electrons,inducing limited ionization and excitation rate.The overshoot phenomenon gradually disappears and the electron density decreases,when the probe moves away from reactor centre.In Ar/CF_(4) discharge,the overshoot phenomenon of electron density is weaker than that in the Ar discharge,and the plasma reaches a steady density within a much shorter time,which is probably due to the more ionization channels and lower ionization thresholds in the Ar/CF_(4) plasma. 展开更多
关键词 pulse inductively coupled plasma OVERSHOOT spatial distribution
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Measurement of transient neutral gas puff pressure in the NUDT_IPPTx by a fast ionization gauge
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作者 Dawei GUO Mousen CHENG +3 位作者 Xiaokang LI Bixuan CHE Xiong YANG Moge WANG 《Plasma Science and Technology》 SCIE EI CAS CSCD 2018年第12期117-124,共8页
A gas injector was designed for the 400 J/pulse prototype of the planar inductive pulsed plasma thruster(IPPT) developed by the National University of Defense Technology(NUDT_IPPTx).As the gas puff distribution ov... A gas injector was designed for the 400 J/pulse prototype of the planar inductive pulsed plasma thruster(IPPT) developed by the National University of Defense Technology(NUDT_IPPTx).As the gas puff distribution over the coil surface is critical to the NUDT_IPPTx functioning efficiently, a fast ionization gauge was developed to investigate the neutral gas pressure profiles to seek the critical time when the thruster is ignited. The gauge was calibrated for argon by using a capacitance manometer. Time-resolved pressure profiles have been acquired in the condition of the gas puff mass matching with the discharge energy and the drive coil parameters of the NUDT_IPPTx. It is demonstrated that the gas injector can supply a gas puff with a sufficiently steep(dp/dt?≈?770 kPa s-1) leading and trailing edge, and the gas puff can be compressed against the drive coil as expected. The critical ignition moment is considered to appear at some instant between 525 μs and 650 μs after the valve trigger. 展开更多
关键词 inductive pulsed plasma thruster gas injection fast ionization gauge fast pulsed valve neutral gas pressure
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