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
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