Presentation 2004/1/16
Status of The Applicability Study on Lithium-ion Cells as Space Powers at JAXA
Xianming Wang, Chisa Yamada, Yoshitsugu Sone, Saburo Kuwajima,
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Abstract(in English) In order to develop lithium-ion cells for space applications, applicability evaluation on 10-100 Ah-class lithium-ion cells is being performed by simulating satellite 's operation at Japan Aerospace Exploration Agency (JAXA). So far, 20.000 cycles for low-Earth-orbit (LEO) and 1,200 cycles for geostationary-Earth-orbit (GEO) satellite simulation testing have been completed. These results respectively correspond to about 3- and 13-year LEO and GEO satellite operations, indicating good applicability of lithium-ion cells as satellite power. The simulation testing of H-IIA transfer vehicle (HTV) operation disclosed that lithium-ion cells were applicable for this short-term mission even with a high charge rate.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) Lithium-ion cells / Satellite / H-IIA transfer vehicle (HTV) / Applicability evaluation
Paper # EE2003-49,CPM2003-154
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Conference Information
Committee EE
Conference Date 2004/1/16(1days)
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Paper Information
Registration To Energy Engineering in Electronics and Communications (EE)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) Status of The Applicability Study on Lithium-ion Cells as Space Powers at JAXA
Sub Title (in English)
Keyword(1) Lithium-ion cells
Keyword(2) Satellite
Keyword(3) H-IIA transfer vehicle (HTV)
Keyword(4) Applicability evaluation
1st Author's Name Xianming Wang
1st Author's Affiliation Spacecraft Electrical Engineering Group, Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency (JAXA)()
2nd Author's Name Chisa Yamada
2nd Author's Affiliation Spacecraft Electrical Engineering Group, Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency (JAXA)
3rd Author's Name Yoshitsugu Sone
3rd Author's Affiliation Spacecraft Electrical Engineering Group, Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency (JAXA)
4th Author's Name Saburo Kuwajima
4th Author's Affiliation Spacecraft Electrical Engineering Group, Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency (JAXA)
Date 2004/1/16
Paper # EE2003-49,CPM2003-154
Volume (vol) vol.103
Number (no) 595
Page pp.pp.-
#Pages 6
Date of Issue