DocumentCode
1338192
Title
A Miniature Inductively Coupled Plasma Source for Ion Thrusters
Author
Browning, Jim ; Lee, Carl ; Plumlee, Don ; Shawver, Sonya ; Loo, Sin Ming ; Yates, Mallory ; McCrink, Matt ; Taff, Jesse
Author_Institution
Electr. & Comput. Eng. Dept., Boise State Univ., Boise, ID, USA
Volume
39
Issue
11
fYear
2011
Firstpage
3187
Lastpage
3195
Abstract
A small inductively coupled plasma source has been developed for use in an ion thruster. A 10.1-mm-diameter thick film silver spiral antenna is fabricated on a low-temperature cofired ceramic with a 35-μm dielectric over the antenna. The antenna has been able to sustain an argon plasma over a frequency range from 448 to 1020 MHz with pressures ranging from 50 mtorr to 1.75 torr. Plasma start powers ranged from 3 to 50 W with minimum sustain powers down to 0.1 W. Antenna electric field measurements have been made in air and compared with simulation of the antenna field using COMSOL. These results show that the antenna pattern is dominated by the standing wave pattern of the spiral antenna. Simulations of the RF power density versus frequency compare well with the plasma start power variation except for a large start power peak between 600 and 700 MHz.
Keywords
UHF antennas; argon; ceramics; ion engines; plasma applications; plasma sources; spiral antennas; Ar; RF power density; antenna electric field measurements; argon plasma; frequency 448 MHz to 1020 MHz; ion thrusters; low temperature cofired ceramic; miniature inductively coupled plasma source; power 3 W to 50 W; pressure 50 mtorr to 1.75 torr; size 10.1 mm; size 35 mum; thick film silver spiral antenna; Antenna measurements; Antennas; Connectors; Iterative closest point algorithm; Plasmas; Radio frequency; Spirals; Inductively coupled plasma (ICP); ion thruster; microplasma;
fLanguage
English
Journal_Title
Plasma Science, IEEE Transactions on
Publisher
ieee
ISSN
0093-3813
Type
jour
DOI
10.1109/TPS.2011.2167634
Filename
6032759
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