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Channel wall sheath thickness in an anode-layer Hall thruster RAIJIN66 wasinvestigated by a two-dimensional hybrid simulation and a one-dimensionalsheath model. A hybrid particle-fluid model with the quasineutrality assumptionwas used to obtain the wall ion flux and plasma property at plasma-sheath edge.The plasma property inside the sheath was estimated by the nonneutral sheathmodel. The simulated ion wall current density at the channel exit was 100 A/m2,and the estimated sheath thickness was 0.64 mm. If the wall ion current densityis reduced to 1/20 of this value, the sheath region will be extended to cover50\% of the channel width.

Sheath Analysis of Conducting Channel Walls in Anode-Layer Hall Thruster with Acceleration Zone Shifted Downstream