Simulation of a capacitively coupled plasma micro-thruster using the particle-in-cell method.
ORAL
Abstract
A radio-frequency (13.56MHz) capacitively coupled plasma (CCP) micro-thruster was simulated in two dimensions by an electrostatic particle-in-cell (PIC) method, using a PPPL-modified version of the commercial LSP code [1]. At the gas valve, the gas pressure is high, up to 5 Torr, and the discharge can operate at high voltages, up to 400 V in argon. Results were benchmarked against the previous 2D fluid simulations of ref. [2] and validated by comparison with the experimental data of ref. [3]. Results show plasma properties depend strongly on the secondary electron emission from walls and dielectric thickness separating electrodes from the plasma. [1] A.T. Powis, J.A. Carlsson, I.D. Kaganovich, Y. Raitses, and A. Smolyakov, \textit{Physics of Plasmas}~\textbf{25}, 072110 (2018). [2] A. Greig, C. Charles, and R. W. Boswell, \textit{Frontiers in Physics}~\textbf{2}, 80 (2015). [3] C. Charles and R. W. Boswell,~\textit{Plasma Sources Sci. Technol~}\textbf{21,~}022002 (2012).
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Authors
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Michael May
Princeton Plasma Physics Laboratory
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Andrew Powis
Princeton Plasma Physics Laboratory, Princeton University, Mechanical and Aerospace Engineering
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Igor Kaganovich
Princeton Plasma Physics Laboratory, PPPL, Princeton Plasma Physics Lab