WEKO3
アイテム
{"_buckets": {"deposit": "1d55bc55-31e8-4772-a0be-4ff8b1f3b2dd"}, "_deposit": {"created_by": 1, "id": "6271", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6271"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006271", "sets": ["1060", "1893"]}, "author_link": ["31584", "31578", "31580", "31586", "31585", "31583", "31579", "31577", "31582", "31581"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Long-term cycle-life testing of large-capacity lithium-ion cells for space applications"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2006-01-20", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "80", "bibliographicPageStart": "77", "bibliographicVolumeNumber": "JAXA-SP-05-008", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術"}, {"bibliographic_title": "JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "In a spacecraft, battery system is one of the most massive onboard components. The specific advantages of lithium-ion technology in energy density and working voltage offer the possibility of huge reductions in battery mass, and hence contribute to lower launch costs and enable missions that have critical weight and/or volume margins. To facilitate the applications of lithium-ion battery in a spacecraft, we began conducting the long-term evaluation on 10-100 Ah-class lithium-ion cells by simulating satellite\u0027s operation in 1998. In this paper, we provide a review of the latest cycle-life test results of these large-capacity lithium-ion cells. Thus far, for some of these cells, we have verified impressive life performance exceeding 29,000 cycles in a Low-Earth-Orbit (LEO) simulation mode and 1,700 cycles in a Geosynchronous-Earth-Orbit (GEO) simulation mode. These results respectively correspond to about 5- and 19-year LEO and GEO satellite operations, indicating good applicability of lithium-ion cells as power storage devices in a satellite. Since the electrode material is an important factor to affect the charge-discharge behavior of a lithium-ion cell, we also compared the cycling performance of lithium-ion cells with different electrode materials.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0049054015", "subitem_description_type": "Other"}]}, "item_3_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: JAXA-SP-05-008", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙航空研究開発機構"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1349-113X", "subitem_source_identifier_type": "ISSN"}]}, "item_3_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AA11984031", "subitem_source_identifier_type": "NCID"}]}, "item_3_text_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "エネルギー生成及び変換"}, {"subitem_text_value": "宇宙船の推進及び出力"}, {"subitem_text_value": "宇宙船設計、試験及び性能"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 特別資料"}]}, "item_3_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: SP"}]}, "item_3_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 7"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "Wang, Xianming"}], "nameIdentifiers": [{"nameIdentifier": "31577", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "内藤, 均"}], "nameIdentifiers": [{"nameIdentifier": "31578", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "山田, 知佐"}], "nameIdentifiers": [{"nameIdentifier": "31579", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "瀬上, 剛"}], "nameIdentifiers": [{"nameIdentifier": "31580", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "岐部, 公一"}], "nameIdentifiers": [{"nameIdentifier": "31581", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Wang, Xianming", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31582", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Naito, Hitoshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31583", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yamada, Chisa", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31584", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Segami, Go", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31585", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kibe, Koichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31586", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "ファイル情報", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2020-01-16"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "49054015.pdf", "filesize": [{"value": "1.0 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1000000.0, "url": {"label": "49054015.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6271/files/49054015.pdf"}, "version_id": "0320e3f1-eaa9-4c85-9400-a72a892b6c46"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "リチウムイオン電池", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衛星機器", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衛星搭載機器", "subitem_subject_scheme": "Other"}, {"subitem_subject": "エネルギー密度", "subitem_subject_scheme": "Other"}, {"subitem_subject": "静止軌道", "subitem_subject_scheme": "Other"}, {"subitem_subject": "長期サイクル寿命試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "放電深度", "subitem_subject_scheme": "Other"}, {"subitem_subject": "低高度地球周回軌道", "subitem_subject_scheme": "Other"}, {"subitem_subject": "グラファイト", "subitem_subject_scheme": "Other"}, {"subitem_subject": "lithium ion battery", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite instrument", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite-borne instrument", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "energy density", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "geostationary orbit", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "long term cycle life testing", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "depth of discharge", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "low Earth orbit", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "graphite", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}]}, "item_language": {"attribute_name": "言語", "attribute_value_mlt": [{"subitem_language": "jpn"}]}, "item_resource_type": {"attribute_name": "資源タイプ", "attribute_value_mlt": [{"resourcetype": "technical report", "resourceuri": "http://purl.org/coar/resource_type/c_18gh"}]}, "item_title": "大型リチウムイオン電池の長期的サイクル寿命特性評価", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "大型リチウムイオン電池の長期的サイクル寿命特性評価"}]}, "item_type_id": "3", "owner": "1", "path": ["1060", "1893"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6271", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6271", "relation": {}, "relation_version_is_last": true, "title": ["大型リチウムイオン電池の長期的サイクル寿命特性評価"], "weko_shared_id": -1}
大型リチウムイオン電池の長期的サイクル寿命特性評価
https://jaxa.repo.nii.ac.jp/records/6271
https://jaxa.repo.nii.ac.jp/records/6271a04c1852-fb78-45ee-b35c-69d27d53c2b6
名前 / ファイル | ライセンス | アクション |
---|---|---|
49054015.pdf (1.0 MB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 大型リチウムイオン電池の長期的サイクル寿命特性評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リチウムイオン電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星機器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星搭載機器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エネルギー密度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 静止軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 長期サイクル寿命試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 放電深度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低高度地球周回軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | グラファイト | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lithium ion battery | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite instrument | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite-borne instrument | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | energy density | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | geostationary orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | long term cycle life testing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | depth of discharge | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low Earth orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | graphite | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Long-term cycle-life testing of large-capacity lithium-ion cells for space applications | |||||
著者 |
Wang, Xianming
× Wang, Xianming× 内藤, 均× 山田, 知佐× 瀬上, 剛× 岐部, 公一× Wang, Xianming× Naito, Hitoshi× Yamada, Chisa× Segami, Go× Kibe, Koichi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems 巻 JAXA-SP-05-008, p. 77-80, 発行日 2006-01-20 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In a spacecraft, battery system is one of the most massive onboard components. The specific advantages of lithium-ion technology in energy density and working voltage offer the possibility of huge reductions in battery mass, and hence contribute to lower launch costs and enable missions that have critical weight and/or volume margins. To facilitate the applications of lithium-ion battery in a spacecraft, we began conducting the long-term evaluation on 10-100 Ah-class lithium-ion cells by simulating satellite's operation in 1998. In this paper, we provide a review of the latest cycle-life test results of these large-capacity lithium-ion cells. Thus far, for some of these cells, we have verified impressive life performance exceeding 29,000 cycles in a Low-Earth-Orbit (LEO) simulation mode and 1,700 cycles in a Geosynchronous-Earth-Orbit (GEO) simulation mode. These results respectively correspond to about 5- and 19-year LEO and GEO satellite operations, indicating good applicability of lithium-ion cells as power storage devices in a satellite. Since the electrode material is an important factor to affect the charge-discharge behavior of a lithium-ion cell, we also compared the cycling performance of lithium-ion cells with different electrode materials. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049054015 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-05-008 |