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日本航空宇宙学会論文集
Vol. 51 (2003) No. 596 P 492-497

記事言語:

http://doi.org/10.2322/jjsass.51.492

論文

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.

Copyright © 2003 The Japan Society for Aeronautical and Space Sciences

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