Investigation of a small, closed electron drift, stationary plasma thruster

被引：10

作者：

Guerrini, G ^{[1
]}

Vesselovzorov, AN ^{[1
]}

Bacal, M ^{[1
]}

Pokrovsky, IB ^{[1
]}

机构：

[1] RRC,KURCHATOV INST,MOSCOW,RUSSIA

来源：

REVIEW OF SCIENTIFIC INSTRUMENTS | 1996年 / 67卷 / 03期

关键词：

D O I：

10.1063/1.1146793

中图分类号：

TH7 [仪器、仪表];

学科分类号：

0804 ; 080401 ; 081102 ;

摘要：

The interest in low-power electric thrusters stimulated our research on a small stationary plasma thruster. The first results on the dependence of the thrust, the discharge current, the ion current, and the axial electron current on gas flow are reported. It was also shown that the drop of the discharge current with magnetic field is strongly affected by the emission current of the filament neutralizer. (C) 1996 American Institute of Physics.

引用

页码：990 / 992

页数：3

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