AIAA Propulsion and Energy 2021 Forum 2021
DOI: 10.2514/6.2021-3414
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A Comparison of 1D Particle-in-Cell and Fluid Models for Hall Effect Thrusters

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Cited by 2 publications
(6 citation statements)
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“…The 1D PIC-MCC simulation code is benchmarked against the Turner test case based on a 1D capacitivelycoupled plasma [35], which is proposed as a benchmark problem in the LTP community. In addition, the present simulation code is benchmarked against two separate PIC-MCC results within the Plasma Dynamics Modeling Laboratory at Stanford University [34,36].…”
Section: A 1d Het Discharge Plasma Modelmentioning
confidence: 99%
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“…The 1D PIC-MCC simulation code is benchmarked against the Turner test case based on a 1D capacitivelycoupled plasma [35], which is proposed as a benchmark problem in the LTP community. In addition, the present simulation code is benchmarked against two separate PIC-MCC results within the Plasma Dynamics Modeling Laboratory at Stanford University [34,36].…”
Section: A 1d Het Discharge Plasma Modelmentioning
confidence: 99%
“…In this model, the anode potential is 300 V and the potential at the cathode line is 0 V. The propellant is xenon and the mass flow rate from the anode is 5 mg s −1 . The maximum magnetic field is 15 mT and the axial profile of the radial magnetic field is used in this study follows the profile shown in references [8,36]. The computational domain is 5 cm and the length of the channel is 2.5 cm.…”
Section: Numerical Parametersmentioning
confidence: 99%
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“…The present 2D axisymmetric simulation is developed based on an in-house, 2D Cartesian PIC code for low-temperature magnetized plasmas [19,20,26,27]. The MCC model used in the present axisymmetric PIC/MCC model is based on another in-house 1D PIC/MCC model [28], which is validated and benchmarked against [18,29].…”
Section: Axisymmetric Pic/mcc Modelmentioning
confidence: 99%