A comparison of emissive probe techniques for electric potential measurements in a complex plasma

被引:111
作者
Sheehan, J. P. [1 ]
Raitses, Y. [2 ]
Hershkowitz, N. [1 ]
Kaganovich, I. [2 ]
Fisch, N. J. [2 ]
机构
[1] Univ Wisconsin, Dept Engn Phys, Madison, WI 53706 USA
[2] Princeton Univ, Princeton Plasma Phys Lab, Princeton, NJ 08543 USA
基金
美国国家科学基金会;
关键词
CHARGE LIMITED EMISSION; LOW-TEMPERATURE PLASMA; FAST TIME EVOLUTIONS; SPACE-CHARGE; ELECTROSTATIC-PROBE; VELOCITY DISTRIBUTION; HALL THRUSTERS; SHEATH; SECONDARY; LANGMUIR;
D O I
10.1063/1.3601354
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
The major emissive probe techniques are compared to better understand the floating potential of an electron emitting surface in a plasma. An overview of the separation point technique, floating point technique, and inflection point in the limit of zero emission technique is given, addressing how each method works as well as the theoretical basis and limitations of each. It is shown that while the floating point method is the most popular, it is expected to yield a value similar to 1.5T(e)/e below the plasma potential due to a virtual cathode forming around the probe. The theoretical predictions were checked with experiments performed in a 2 kW annular Hall thruster plasma (n(e) similar to 10(9)-10(10) cm(-3) and T-e similar to 10-50 eV). The authors find that the floating point method gives a value around 2T(e)/e below the inflection point method, which is shown to be a more accurate emissive probe technique than other techniques used in this work for measurements of the plasma potential. (C) 2011 American Institute of Physics. [doi: 10.1063/1.3601354]
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页数:9
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