DocumentCode
2633822
Title
Design of a new discharge power supply for ion engine
Author
Nagano, Hiroshi ; Kajiwara, Kenichi ; Osuga, Hiroyuki ; Ozaki, Toshiyuki ; Shuto, Kazuo
Author_Institution
Aerosp. R&D Directorate, Japan Aerosp. Exploration Agency, Tsukuba, Japan
fYear
2010
fDate
6-8 Sept. 2010
Abstract
JAXA has researched the Super Low Altitude Test Satellite (SLATS) for next generation earth observing satellite. We started research and development of a new IES in order to apply for the SLATS program. In this paper, we describe the preliminary design results of the IES configuration plan for the SLATS, performance requirements of the power processing control unit (PPCU) and the developments results of the bread board of model (BBM) of this discharge power supply.
Keywords
aircraft power systems; artificial satellites; ion engines; JAXA; SLATS program; bread board of model; discharge power supply; ion engine; next generation earth observing satellite; power processing control unit; super low altitude test satellite; Discharges; Engines; Power conversion; Power supplies; Satellites; Voltage control; Aerospace; Converter circuit; Design; Optimal control; Power supply;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics and Motion Control Conference (EPE/PEMC), 2010 14th International
Conference_Location
Ohrid
Print_ISBN
978-1-4244-7856-9
Type
conf
DOI
10.1109/EPEPEMC.2010.5606911
Filename
5606911
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