DocumentCode :
3208055
Title :
Modeling the characteristics of an inductively coupled plasma antenna for use in a micro-propulsion system
Author :
Shawver, Sonya ; Browning, Jim
Author_Institution :
Dept. of Electr. & Comput. Eng., Boise State Univ., Boise, India
fYear :
2012
fDate :
5-8 Aug. 2012
Firstpage :
1040
Lastpage :
1043
Abstract :
An ion thruster for small satellites is under development. The thruster uses an Inductively Coupled Plasma (ICP) generated by a flat spiral antenna for the ion source. The antenna is fabricated using the Low Temperature Co-Fired Ceramic (LTCC) materials system. The antenna has been modeled using COMSOL Multiphysics® simulation software. The antenna operating frequency range (600 MHz to 1 GHz) in LTCC (εr=7.8) results in a wavelength on the same order of magnitude as the total length of conductor in the antenna. An analysis of the antenna´s behavior is presented.
Keywords :
antennas in plasma; artificial satellites; ion engines; ion sources; plasma devices; plasma simulation; plasma sources; plasma temperature; propulsion; COMSOL Multiphysics® simulation software; antenna behavior analysis; antenna conductor length; antenna operating frequency range; flat spiral antenna; frequency 600 MHz to 1 GHz; inductively coupled plasma antenna characteristics; inductively coupled plasma generation; ion source; ion thruster; low temperature Co-fired ceramic material system; micropropulsion system; Antenna measurements; Antennas; Electric fields; Magnetic field measurement; Plasmas; Radio frequency; Spirals;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Circuits and Systems (MWSCAS), 2012 IEEE 55th International Midwest Symposium on
Conference_Location :
Boise, ID
ISSN :
1548-3746
Print_ISBN :
978-1-4673-2526-4
Electronic_ISBN :
1548-3746
Type :
conf
DOI :
10.1109/MWSCAS.2012.6292201
Filename :
6292201
Link To Document :
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