Storage of a lithium-ion secondary battery under micro-gravity conditions

Yoshitsugu Sone; Hiroki Ooto; Masahiro Yamamoto; Takashi Eguro; Shigeru Sakai; Teiji Yoshida; Keiji Takahashi; Masatoshi Uno; Kazuyuki Hirose; Michio Tajima; Jun'ichiro Kawaguchi

doi:10.1016/j.jpowsour.2008.02.060

Storage of a lithium-ion secondary battery under micro-gravity conditions

Yoshitsugu Sone^*, Hiroki Ooto, Masahiro Yamamoto, Takashi Eguro, Shigeru Sakai, Teiji Yoshida, Keiji Takahashi, Masatoshi Uno, Kazuyuki Hirose, Michio Tajima, Jun'ichiro Kawaguchi

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

13 Citations (Scopus)

Abstract

'HAYABUSA' is a Japanese inter-planetary spacecraft built for the exploration of an asteroid named 'ITOKAWA.' The spacecraft is powered by a 13.2 Ah lithium-ion secondary battery. To realize maximum performance of the battery for long flight operation, the state-of-charge (SOC) of the battery was maintained at ca. 65% during storage, in case it is required for a loss of attitude control. The capacity of the battery was measured during flight operations. Along with the operation in orbit, a ground-test battery was discharged, and both results showed a good agreement. This result confirmed that the performance of the lithium-ion secondary battery stored under micro-gravity conditions is predictable using a ground-test battery.

Original language	English
Pages (from-to)	149-154
Number of pages	6
Journal	Journal of Power Sources
Volume	181
Issue number	1
DOIs	https://doi.org/10.1016/j.jpowsour.2008.02.060
Publication status	Published - 15 Jun 2008
Externally published	Yes

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10.1016/j.jpowsour.2008.02.060

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title = "Storage of a lithium-ion secondary battery under micro-gravity conditions",

abstract = "'HAYABUSA' is a Japanese inter-planetary spacecraft built for the exploration of an asteroid named 'ITOKAWA.' The spacecraft is powered by a 13.2 Ah lithium-ion secondary battery. To realize maximum performance of the battery for long flight operation, the state-of-charge (SOC) of the battery was maintained at ca. 65\% during storage, in case it is required for a loss of attitude control. The capacity of the battery was measured during flight operations. Along with the operation in orbit, a ground-test battery was discharged, and both results showed a good agreement. This result confirmed that the performance of the lithium-ion secondary battery stored under micro-gravity conditions is predictable using a ground-test battery.",

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author = "Yoshitsugu Sone and Hiroki Ooto and Masahiro Yamamoto and Takashi Eguro and Shigeru Sakai and Teiji Yoshida and Keiji Takahashi and Masatoshi Uno and Kazuyuki Hirose and Michio Tajima and Jun'ichiro Kawaguchi",

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language = "English",

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T1 - Storage of a lithium-ion secondary battery under micro-gravity conditions

AU - Sone, Yoshitsugu

AU - Ooto, Hiroki

AU - Yamamoto, Masahiro

AU - Eguro, Takashi

AU - Sakai, Shigeru

AU - Yoshida, Teiji

AU - Takahashi, Keiji

AU - Uno, Masatoshi

AU - Hirose, Kazuyuki

AU - Tajima, Michio

AU - Kawaguchi, Jun'ichiro

PY - 2008/6/15

Y1 - 2008/6/15

N2 - 'HAYABUSA' is a Japanese inter-planetary spacecraft built for the exploration of an asteroid named 'ITOKAWA.' The spacecraft is powered by a 13.2 Ah lithium-ion secondary battery. To realize maximum performance of the battery for long flight operation, the state-of-charge (SOC) of the battery was maintained at ca. 65% during storage, in case it is required for a loss of attitude control. The capacity of the battery was measured during flight operations. Along with the operation in orbit, a ground-test battery was discharged, and both results showed a good agreement. This result confirmed that the performance of the lithium-ion secondary battery stored under micro-gravity conditions is predictable using a ground-test battery.

AB - 'HAYABUSA' is a Japanese inter-planetary spacecraft built for the exploration of an asteroid named 'ITOKAWA.' The spacecraft is powered by a 13.2 Ah lithium-ion secondary battery. To realize maximum performance of the battery for long flight operation, the state-of-charge (SOC) of the battery was maintained at ca. 65% during storage, in case it is required for a loss of attitude control. The capacity of the battery was measured during flight operations. Along with the operation in orbit, a ground-test battery was discharged, and both results showed a good agreement. This result confirmed that the performance of the lithium-ion secondary battery stored under micro-gravity conditions is predictable using a ground-test battery.

KW - Aerospace

KW - In-orbit

KW - Lithium-ion secondary cell

KW - Micro-gravity

KW - Satellite

KW - Spacecraft

UR - https://www.scopus.com/pages/publications/43049165762

U2 - 10.1016/j.jpowsour.2008.02.060

DO - 10.1016/j.jpowsour.2008.02.060

M3 - Article

AN - SCOPUS:43049165762

SN - 0378-7753

VL - 181

SP - 149

EP - 154

JO - Journal of Power Sources

JF - Journal of Power Sources

IS - 1

ER -

Storage of a lithium-ion secondary battery under micro-gravity conditions

Abstract

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