DocumentCode :
4412
Title :
Experimental Visualization of Ion Thruster Neutralization Phenomena
Author :
Nakayama, Yoshinori ; Tanaka, Futoshi
Author_Institution :
Nat. Defense Acad. of Japan, Yokosuka, Japan
Volume :
43
Issue :
1
fYear :
2015
fDate :
Jan. 2015
Firstpage :
269
Lastpage :
276
Abstract :
Understanding of neutralization phenomena is important to develop ion thrusters with higher efficiency and durability. A 2-D ion thruster with a miniature microwave neutralizer was visualized in this paper to investigate neutralization phenomena. The thruster can emit bright sheet-shaped ion beams. The neutralizer current can be controlled by the supplied microwave power. Observation of the downstream region and measurements of the currents and potential confirmed that insufficient neutralizer current increased the ion beamwidth, space potential increase in the downstream region, and semicircular luminescence zone formation in the region. These phenomena imply the 2-D formation of a virtual anode in the downstream region of the grid system, and indicate that 2-D or 3-D evaluations are necessary to elucidate neutralization phenomena.
Keywords :
aerospace propulsion; durability; electric propulsion; ion beams; ion engines; 2D evaluations; 2D ion thruster; 3D evaluations; bright sheet-shaped ion beams; current measurements; durability; electric propulsion; grid system downstream region; ion beamwidth; ion thruster neutralization phenomena visualization; microwave power; miniature microwave neutralizer; neutralizer current; semicircular luminescence zone formation; space potential; virtual anode; Acceleration; Anodes; Current measurement; Electric potential; Ion beams; Microwave measurement; Visualization; Electric propulsion; ion beam optics; ion thruster; neutralization; virtual anode; virtual anode.;
fLanguage :
English
Journal_Title :
Plasma Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-3813
Type :
jour
DOI :
10.1109/TPS.2014.2321418
Filename :
6814950
Link To Document :
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