We present a model for electron transport across the magnetic field of a Hall thruster and integrate this model into 2-D hybrid particle-in-cell simulations. The model is based on a simple scaling of the turbulent electron energy dissipation rate and the assumption that this dissipation results in Ohmic heating. Implementing the model into 2-D hybrid simulations is straightforward and leverages the existing framework for solving the electron fluid equations. The model recovers the axial variation in the mobility seen in experiments, predicting the generation of a transport barrier which anchors the region of plasma acceleration. The predicted xenon neutral and ion velocities are found to be in good agreement with laser-induced fluorescence measurements. (C) 2015 AIP Publishing LLC.
机构:
Indian Inst Technol Madras, Dept Aerosp Engn, Chennai 132001, Tamil Nadu, IndiaIndian Inst Technol Madras, Dept Aerosp Engn, Chennai 132001, Tamil Nadu, India
Sandhu, Jatinder Pal Singh
Ghosh, Santanu
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Indian Inst Technol Madras, Dept Aerosp Engn, Chennai 132001, Tamil Nadu, IndiaIndian Inst Technol Madras, Dept Aerosp Engn, Chennai 132001, Tamil Nadu, India