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arXiv · 2312.09569

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

Rei Kawashima
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Abstract

Channel wall sheath thickness in an anode-layer Hall thruster RAIJIN66 was investigated by a two-dimensional hybrid simulation and a one-dimensional sheath model. A hybrid particle-fluid model with the quasineutrality assumption was 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 sheath model. 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 density is reduced to 1/20 of this value, the sheath region will be extended to cover 50\% of the channel width.

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Rei Kawashima. 2023-12-15. Sheath Analysis of Conducting Channel Walls in Anode-Layer Hall Thruster with Acceleration Zone Shifted Downstream. https://arxiv.org/abs/2312.09569

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