《Table 2.Mode arrangements of simulation cases.》

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《Three-dimensional particle simulation of ion thruster plume flows with EX-PWS》

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Figure 1 shows the boundary definitions in the meantime.The grid used in this study includes four thruster exit planes，walls of the thruster，and the computational domain boundaries.The computational domain boundaries are regard as free boundaries for all kinds of particles.The treatment of electric field on the boundaries is interpolation.The exit planes are the sources of particles and specular reflection boundaries for the striking particles.The thruster walls are diffuse reflection boundaries and neutralize ions simultaneously.The electric potentials of exit planes and thruster walls are equal to zero，and the temperatures are equal to 300 K.