In an effort to temporally resolve the electron density, electron temperature, and plasma potential for turbulent plasma discharges, a unique high-speed dual Langmuir probe (HDLP) has been developed. A traditional single Langmuir probe of cylindrical geometry (exposed to the plasma) is swept simultaneously with a nearby capacitance and noise compensating null probe (fully insulated from the plasma) to enable bias sweep rates on a microsecond timescale. Traditional thin-sheath Langmuir probe theory is applied for interpretation of the collected probe data. Data at a sweep rate of 100 kHz are presented; however the developed system is capable of running at 1 MHz—near the upper limit of the applied electrostatic Langmuir probe theory for the investigated plasma conditions. Large sets (100 000 sweeps at each of 352 spatial locations) of contiguous turbulent plasma properties are collected using simple electronics for probe bias driving and current measurement attaining 80 dB signal-to-noise measurements with dc to 1 MHz bandwidth. Near- and far-field plume measurements with the HDLP system are performed downstream from a modern Hall effect thruster where the time-averaged plasma properties exhibit the approximate ranges: electron density from , electron temperature from 1 to 3.5 eV, and plasma potential from 5 to 15 V. The thruster discharge of 200 V (constant anode potential) and 2 A (average discharge current) displays strong, 2.2 A peak-to-peak, current oscillations at 19 kHz, characteristic of the thruster “breathing mode” ionization instability. Large amplitude discharge current fluctuations are typical for most Hall thrusters, yet the HDLP system reveals the presence of the same 19 kHz fluctuations in , , and throughout the entire plume with peak-to-peak divided by mean plasma properties that average 94%. The propagation delays between the discharge current fluctuations and the corresponding plasma density fluctuations agree well with expected ion transit-times observed with distinct plasma waves traveling away from the thruster at velocities .
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July 2010
Research Article|
July 15 2010
High-speed dual Langmuir probe
Robert B. Lobbia;
Robert B. Lobbia
Department of Aerospace Engineering, Plasmadynamics and Electric Propulsion Laboratory,
The University of Michigan
, Ann Arbor, Michigan 48109, USA
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Alec D. Gallimore
Alec D. Gallimore
Department of Aerospace Engineering, Plasmadynamics and Electric Propulsion Laboratory,
The University of Michigan
, Ann Arbor, Michigan 48109, USA
Search for other works by this author on:
Rev. Sci. Instrum. 81, 073503 (2010)
Article history
Received:
November 24 2009
Accepted:
May 23 2010
Citation
Robert B. Lobbia, Alec D. Gallimore; High-speed dual Langmuir probe. Rev. Sci. Instrum. 1 July 2010; 81 (7): 073503. https://doi.org/10.1063/1.3455201
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