中文摘要：

为进一步揭示霍尔推力器放电通道饱和电子温度高达50—60eV的原因，利用二维粒子模拟方法研究了霍尔推力器中电子温度各向异性对等离子体与壁面相互作用的影响，统计了等离子体与壁面相互作用的重要物理量，如电子与壁面的碰撞频率、通道电子在壁面的能量沉积及二次电子对通道电子的冷却．结果表明，当电子温度较低时。电子温度各向异性对等离子体与壁面相互作用的影响较小；当电子温度大于24eV时，等离子体与壁面相互作用明显增强，并且电子温度各向异性会显著地降低电子与壁面的碰撞频率，减小电子在壁面的能量沉积，减弱鞘层对通道电子的冷却效应．电子温度的各向异性通过减弱通道电子与壁面的相互作用，有利于提高霍尔推力器放电通道的饱和电子温度．

英文摘要：

To further reveal the physical mechanism of the saturated electron temperature which is about 50--60 eV in the discharge channel of Hall thruster, the effect of electron temperature anisotropy （ETA） on plasma-wall interaction in Hall thruster is studied by using a 2D3V particle-in-cell sheath dynamic model. Some important physical parameters such as electron-wall collision frequency, electron energy deposition at wall and the cooling effect of near-wall sheath on channel electron are calculated. Numerical results indicate that the influence of ETA on plasma-wall interaction is neglectable when electron temperature is low. However, when Te 〉 24 eV, the ETA can significantly reduce electron-wall collision frequency, thereby reducing the electron energy deposition at wall and weakening the cooling effect of near-wall sheath on channel electron. It suggests that the anisotropy of electron temperature tends to increase the saturated electron temperature in the discharge channel of Hall thruster through remarkably weakening the interaction between channel electron and wall.