Ion source based on a circular anode layer plasma thruster

被引：2
|
作者：
Gushenets, Vasily [1 ]
Bugaev, Alexey [2 ]
Oks, Efim [1 ,2 ]
机构：
[1] Russian Acad Sci, Siberian Branch, Inst High Current Elect, Tomsk 634055, Russia
[2] Tomsk State Univ Control Syst & Radioelect, Tomsk 634050, Russia
来源：
REVIEW OF SCIENTIFIC INSTRUMENTS | 2019年 / 90卷 / 11期
基金：
俄罗斯基础研究基金会;
关键词：
Acceleration gap - Anode layers - Discharge currents - High currents - Inner surfaces - Plasma thrusters - Pulsed ion sources;
D O I：
10.1063/1.5127095
中图分类号：
TH7 [仪器、仪表];
学科分类号：
0804 ; 080401 ; 081102 ;
摘要：
A new version of pulsed ion source based on plasma thruster technology has been developed and tested. The ion source design uses a circular anode layer geometry in which the ion beam is extracted radially from the full circumference. The source has been tested for operation in argon, nitrogen, and air at a gas flow rate of up to 20 SCCM with discharge current and voltage measurements in low- and high-current modes. The source, having a simple design and open acceleration gap geometry for observation and photography, is suitable for the treatment of the inner surfaces of pipes and tubes. Published under license by AIP Publishing.
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收藏
页数：4
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