Abstract
For the improvement of the performance of a miniature microwave discharge neutralizer, the dependencies of the performance of a neutralizer on the microwave frequency, magnetic field strength, antenna length among other factors were investigated. Extracted electron current strongly depends on magnetic field strength and microwave fre-quency, and the optimal magnetic field depends on the operational condition. Overall, extracted electron current was achieved 19 mA at xenon mass flow rate of 5 µg/s, incident microwave power of 2 W and collector applied voltage of 30 V. The demonstrated performance is enough for practical use as a 30 W class microwave discharge ion engine for 50 kg class satellites.
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CITATION STYLE
YAMAMOTO, N., HIRAOKA, Y., & NAKASHIMA, H. (2014). Development of a Miniature Microwave Discharge Neutralizer for Miniature Ion Engines. JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 62(4), 123–128. https://doi.org/10.2322/jjsass.62.123
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