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Updated: Aug 4, 2025

Low-energy Cathodoluminescence for OxyNitride Phosphors
Published on: November 15, 2016
Heaterless 300 A lanthanum hexaboride hollow cathode
Dan M Goebel1, Adele R Payman1
1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109, USA.
Abstract:
Hollow cathodes used in electric propulsion typically have an external heater to raise the thermionic electron emitter to emission temperatures. Heaterless hollow cathodes that are heated by a Paschen discharge have been historically limited to low discharge currents (<5 A) due to arcing and inefficient heating. A new heaterless technology was previously developed for cathodes up to 50 A, utilizing a refractory metal tube to extend the gas feed line partway into the thermionic insert region. A high voltage (>700 V) Paschen discharge is ignited between the keeper and the tube, which quickly transitions to a lower voltage (<80 V) thermionic discharge from the inner tube surface and heats the thermionic insert by radiation. This "tube-radiator" configuration eliminates arcing and inhibits the long-path-length discharge between the keeper and gas feed tube upstream of the cathode insert that caused inefficient heating in prior designs. This paper describes extending this technology developed for a 50 A cathode to one that is capable of 300 A. The larger cathode uses a 5-mm diameter tantalum tube-radiator and a 6-A, 5-min ignition sequence. Ignition was challenging because the high heating power required (≥300 W) is difficult to maintain with the low voltage (<20 V) keeper discharge that exists prior to igniting the thruster discharge. To achieve self-heating from the lower voltage keeper discharge, the keeper current is raised to 10 A once the LaB6 insert starts emitting. This work shows that the novel tube-radiator heater is scalable to large cathodes capable of tens of thousands of ignitions.

