Thrust performance and stable operation conditions of an anode layer type Hall thruster was investigated using a 1.5kW class anode layer type Hall thruster. The thrust efficiency reached at 53% with the specific impulse of 2,000s, which are competitive with these of SPT-100 thrusters. Anode shape and axial position of the anode were changed. Stability of the discharge was found sensitive to the anode configuration and applied magnetic flux density.
雑誌名
日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
アノードレイヤ型ホールスラスタの作動特性
JSASS_51_596.pdf
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