DocumentCode :
182205
Title :
Scandate hollow cathode for ion thruster
Author :
Vancil, Bernard ; Schmidt, Volker ; Lorr, John ; Ohlinger, Wayne
Author_Institution :
e Beam Inc., Beaverton, OR, USA
fYear :
2014
fDate :
22-24 April 2014
Firstpage :
57
Lastpage :
58
Abstract :
A hollow cathode was fabricated from scandium oxide-doped one-micron tungsten powder. The prepared powder was pressed into a solid billet and sintered in hydrogen. The sintered billet was electron discharge machined to create the hollow emitter. A unique test vehicle was developed consisting of a central wire as anode, a glass-rodded support structure, and a glass envelope, pumped and baked at 400o C. The cathode was tested in both vacuum and one torr of xenon. The vacuum was maintained with barium getters flashed on the internal surface of the envelope. A capsule containing xenon was enclosed in the vacuum envelope. After vacuum testing, the capsule was broken and cathode emission in a xenon discharge was measured. About 2 amps/cm2 space-charge-limited emission was achieved in vacuum at 945o Cb(W). In xenon, the current was 50 amps (17A/cm2) temperature-limited at 880o Cb(W). By contrast, an all-tungsten emitter of the same geometry required a temperature of 1080o Cb(W) to achieve the same current.
Keywords :
cathodes; ion engines; scandium compounds; semiconductor doping; sintering; tungsten; electron discharge machined; glass envelope; glass-rodded support structure; hollow emitter; hydrogen sintered; ion thruster; scandate hollow cathode; scandium oxide-doped one-micron tungsten powder; sintered billet; solid billet; space-charge-limited emission; temperature 400 degC; vacuum envelope; Cathodes; Discharges (electric); Glass; Powders; Tungsten; Vehicles; Xenon; Scandate hollow cathode; ion propulsion;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Vacuum Electronics Conference, IEEE International
Conference_Location :
Monterey, CA
Type :
conf
DOI :
10.1109/IVEC.2014.6857488
Filename :
6857488
Link To Document :
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