TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN
Online ISSN : 1347-3840
ISSN-L : 1347-3840
b) Electric and Advanced Propulsion
Hollow Cathode Studies for the Next Generation Ion Engines in JAXA
Yasushi OHKAWAYukio HAYAKAWAHideki YOSHIDAKatsuhiro MIYAZAKIShoji KITAMURAKenichi KAJIWARA
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2009 年 7 巻 ists26 号 p. Pb_23-Pb_28

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The current status of experimental studies of hollow cathodes for the next-generation ion engines in the Aerospace Research and Development Directorate, JAXA is described. One of the topics on the hollow cathode studies is a life test of a discharge cathode. The keeper disk, orifice plate, and cathode tube of this discharge cathode are made of "high density graphite," which possesses much higher tolerance to ion impingement compared with conventional metal materials. The life test had started in March 2006 and the cumulative operation time reached 15,600 hours in April 2008. No severe degradation has been found both in the operation voltages and electrodes so far, and the test is favorably in progress. In addition to the life test of the discharge cathode, some experiments for design optimization of neutralizer cathodes have been performed. A life test of the neutralizer cathode is being started in June 2008.

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© 2009 The Japan Society for Aeronautical and Space Sciences
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