Triple Langmuir probe measurements in the plume and backflow region of a pulsed plasma thruster

2001 ◽  
Author(s):  
Lawrence Byrne ◽  
Nikolaos Gatsonis ◽  
Eric Pencil
Keyword(s):  
Langmuir Probe ◽  
Pulsed Plasma ◽  
Pulsed Plasma Thruster ◽  
Plasma Thruster ◽  
Langmuir Probe Measurements ◽  
Probe Measurements

Triple Langmuir Probe Measurements in the Plume of a Pulsed Plasma Thruster

2001 ◽  
Vol 17 (4) ◽  
pp. 762-771 ◽  
Author(s):  
Robert Eckman ◽  
Lawrence Byrne ◽  
Nikolaos A. Gatsonis ◽  
Eric J. Pencil
Keyword(s):  
Langmuir Probe ◽  
Pulsed Plasma ◽  
Pulsed Plasma Thruster ◽  
Plasma Thruster ◽  
Langmuir Probe Measurements ◽  
Probe Measurements

Triple Langmuir probe measurements in the plume of a pulsed plasma thruster

1998 ◽  
Author(s):  
Robert Eckman ◽  
Lawrence Byrne ◽  
Edward Cameron ◽  
Nikos Gatsonis ◽  
Eric Pencil
Keyword(s):  
Langmuir Probe ◽  
Pulsed Plasma ◽  
Pulsed Plasma Thruster ◽  
Plasma Thruster ◽  
Langmuir Probe Measurements ◽  
Probe Measurements

Study on the Plume Characteristics of Pulsed Plasma Thruster

2013 ◽  
Vol 347-350 ◽  
pp. 55-58
Author(s):  
Yong Li ◽  
Rui Zhang ◽  
Jian Hua Zong
Keyword(s):  
Electron Temperature ◽  
Langmuir Probe ◽  
Current Model ◽  
Energy Levels ◽  
Pulsed Plasma ◽  
Discharge Energy ◽  
Pulsed Plasma Thruster ◽  
Plasma Thruster ◽  
A Current ◽  
Date Processing

A current-model Triple Langmuir probe was developed and used to measure electron temperature and density of the Pulsed Plasma Thruster plume. To decreasing the errors in measurement, Probe, collection circuit and glow cleaning devices were elaborately designed. A FIR digital Filter based on Matlab was designed and the software for date processing was developed by Labview. Measurements were taken at various position in the plume of a Pulsed Plasma Thruster operating at discharge energy of 6-24J. The results show the thruster plume has electron temperatures in the range between 0.6and 5.4eV, electron densities between 0.9×1019 and 4.1x1021m-3 for all discharge energy levels considered. Electron temperature and density decrease with increasing angle away from the centerline and with decreasing discharge energy.

Volumetric Langmuir probe mapping of a transient pulsed plasma thruster plume

2020 ◽  
Vol 22 (9) ◽  
pp. 094010
Author(s):  
William Yeong Liang LING ◽  
Shuai LIU ◽  
Xiangyang LIU ◽  
Zhiwen WU ◽  
Ningfei WANG
Keyword(s):  
Langmuir Probe ◽  
Pulsed Plasma ◽  
Pulsed Plasma Thruster ◽  
Plasma Thruster ◽  
Probe Mapping
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