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Analysis on discharge process of a plasma-jet triggered gas spark switch 被引量:4
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作者 铁维昊 孟萃 +2 位作者 张雨婷 闫自让 张乔根 《Plasma Science and Technology》 SCIE EI CAS CSCD 2018年第1期59-66,共8页
The plasma-jet triggered gas switch (PJTGS) could operate at a low working coefficient with a low jitter. We observed and analyzed the discharge process of the PJTGS at the lowest working coefficient of 47% with the... The plasma-jet triggered gas switch (PJTGS) could operate at a low working coefficient with a low jitter. We observed and analyzed the discharge process of the PJTGS at the lowest working coefficient of 47% with the trigger voltage of 40 kV and the pulse energy of 2 J to evaluate the effect of the plasma jet. The temporal and spatial evolution and the optical emission speclrum of the plasma jet were captured. And the spraying delay time and outlet velocity under different gas pressures were investigated. In addition, the particle in cell with Monte Carlo collision was employed to obtain the particle distribution of the plasma jet varying with time. The results show that, the plasma jet generated by spark discharge is sprayed into a spark gap within tens of nanoseconds, and its outlet velocity could reach 104 m s-1. The plasma jet plays a non-penetrating inducing role in the triggered discharge process of the PJTGS. On the one hand, the plasma jet provides the initial electrons needed by the discharge; on the other hand, a large number of electrons focusing on the head of the plasma jet distort the electric field between the head of the plasma jet and the opposite electrode. Therefore, a fast discharge originated from the plasma jet is induced and quickly bridges two electrodes. 展开更多
关键词 spark gap plasma jet triggered discharge
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Study on the plasma generation characteristics of an induction-triggered coaxial pulsed plasma thruster
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作者 崔伟胜 刘文正 +1 位作者 田甲 陈修阳 《Plasma Science and Technology》 SCIE EI CAS CSCD 2018年第2期13-18,共6页
At present,spark plugs are used to trigger discharge in pulsed plasma thrusters(PPT),which are known to be life-limiting components due to plasma corrosion and carbon deposition.A strong electric field could be form... At present,spark plugs are used to trigger discharge in pulsed plasma thrusters(PPT),which are known to be life-limiting components due to plasma corrosion and carbon deposition.A strong electric field could be formed in a cathode triple junction(CTJ) to achieve a trigger function under vacuum conditions.We propose an induction-triggered electrode structure on the basis of the CTJ trigger principle.The induction-triggered electrode structure could increase the electric field strength of the CTJ without changing the voltage between electrodes,contributing to a reduction in the electrode breakdown voltage.Additionally,it can maintain the plasma generation effect when the breakdown voltage is reduced in the discharge experiments.The induction-triggered electrode structure could ensure an effective trigger when the ablation distance of Teflon increases,and the magnetic field produced by the discharge current could further improve the plasma density and propagation velocity.The induction-triggered coaxial PPT we propose has a simplified trigger structure,and it is an effective attempt to optimize the micro-satellite thruster. 展开更多
关键词 pulsed plasma thruster cathode triple junction discharge characteristics trigger structure
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