10000-Ignition-Cycle Investigation of a LaB 6 Hollow Cathode for 3-5-Kilowatt Hall Thruster
In this Paper a newly designed heaterless LaB6 hollow cathode is studied for 10,000 ignition cycles. The current-voltage characteristics and upstream pressure of the hollow cathode are monitored during this procedure, and a destructive analysis is made after 10,000 ignition cycles. It is found that...
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Veröffentlicht in: | Journal of propulsion and power 2019-01, Vol.35 (1), p.87 |
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Hauptverfasser: | , , , , , , |
Format: | Artikel |
Sprache: | eng |
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