WEKO3
アイテム
{"_buckets": {"deposit": "ec435301-c9b7-480b-b581-bf6573a6d72d"}, "_deposit": {"created_by": 1, "id": "8121", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "8121"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00008121", "sets": ["1578", "1891"]}, "author_link": ["44882", "44883", "44880", "44885", "44884", "44881"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Space application of thin-film solar cell"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-06", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "25", "bibliographicPageStart": "21", "bibliographic_titles": [{"bibliographic_title": "第23回宇宙エネルギーシンポジウム 平成15年度"}, {"bibliographic_title": "The 23rd ISAS Space Energy Symposium March 9, 2004", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "As growth in electric power of spacecraft, development of less-expensive and lighter space power system is required. Especially, for future high power spacecraft such as the hybrid solar sail that has the potential to explore the Jupiter and asteroids, or Solar Power Satellite, very light weight photovoltaic solar array system with specific power exceeding 1 kW/kg will be required. It is expected to reduce the mass of the solar array system dramatically utilizing the thin-film solar cells. Recently, as low-cost solar cell, amorphous silicon (a-Si) solar cells and CIGS solar cells are developed for the terrestrial commercial product conducted by New Energy and Industrial Technology Development Organization. In addition, high radiation tolerant of CIGS and a-Si solar cells was reported. In this paper, possibility of the terrestrial thin-film solar cell \u0027s technologies for space applications is described.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0047275005", "subitem_description_type": "Other"}]}, "item_5_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙航空研究開発機構宇宙科学研究本部"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]}, "item_5_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": "宇宙船計装"}]}, "item_5_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: シンポジウム・研究会"}]}, "item_5_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: IS"}]}, "item_5_text_42": {"attribute_name": "シンポジウム区分", "attribute_value_mlt": [{"subitem_text_value": "シンポジウム区分: 002"}]}, "item_5_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_5_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部"}]}, "item_5_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 and Astronautical Science"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]}, "item_access_right": {"attribute_name": "アクセス権", "attribute_value_mlt": [{"subitem_access_right": "metadata only access", "subitem_access_right_uri": "http://purl.org/coar/access_right/c_14cb"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "田中, 孝治"}], "nameIdentifiers": [{"nameIdentifier": "44880", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "佐々木, 進"}], "nameIdentifiers": [{"nameIdentifier": "44881", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "川口, 淳一郎"}], "nameIdentifiers": [{"nameIdentifier": "44882", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Tanaka, Koji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44883", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sasaki, Susumu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44884", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kawaguchi, Junichiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44885", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "薄膜太陽電池", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ポリイミド樹脂", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ソーラーパドル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "アモルファスシリコン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "レーザーパターニング", "subitem_subject_scheme": "Other"}, {"subitem_subject": "耐放射線性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "航空宇宙環境", "subitem_subject_scheme": "Other"}, {"subitem_subject": "太陽発電衛星", "subitem_subject_scheme": "Other"}, {"subitem_subject": "thin-film solar cell", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "polyimide resin", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "solar paddle", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "amorphous silicon", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "laser patterning", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "radiation hardening", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerospace environment", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "solar power satellite", "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": "conference paper", "resourceuri": "http://purl.org/coar/resource_type/c_5794"}]}, "item_title": "薄膜太陽電池の宇宙応用", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "薄膜太陽電池の宇宙応用"}]}, "item_type_id": "5", "owner": "1", "path": ["1578", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/8121", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "8121", "relation": {}, "relation_version_is_last": true, "title": ["薄膜太陽電池の宇宙応用"], "weko_shared_id": -1}
薄膜太陽電池の宇宙応用
https://jaxa.repo.nii.ac.jp/records/8121
https://jaxa.repo.nii.ac.jp/records/812179904710-5dc1-475f-a10e-9e8ade33cdcf
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 薄膜太陽電池の宇宙応用 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 薄膜太陽電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ポリイミド樹脂 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ソーラーパドル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アモルファスシリコン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レーザーパターニング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 耐放射線性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空宇宙環境 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽発電衛星 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thin-film solar cell | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | polyimide resin | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar paddle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | amorphous silicon | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laser patterning | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | radiation hardening | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerospace environment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar power satellite | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Space application of thin-film solar cell | |||||
著者 |
田中, 孝治
× 田中, 孝治× 佐々木, 進× 川口, 淳一郎× Tanaka, Koji× Sasaki, Susumu× Kawaguchi, Junichiro |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
第23回宇宙エネルギーシンポジウム 平成15年度 en : The 23rd ISAS Space Energy Symposium March 9, 2004 p. 21-25, 発行日 2004-06 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | As growth in electric power of spacecraft, development of less-expensive and lighter space power system is required. Especially, for future high power spacecraft such as the hybrid solar sail that has the potential to explore the Jupiter and asteroids, or Solar Power Satellite, very light weight photovoltaic solar array system with specific power exceeding 1 kW/kg will be required. It is expected to reduce the mass of the solar array system dramatically utilizing the thin-film solar cells. Recently, as low-cost solar cell, amorphous silicon (a-Si) solar cells and CIGS solar cells are developed for the terrestrial commercial product conducted by New Energy and Industrial Technology Development Organization. In addition, high radiation tolerant of CIGS and a-Si solar cells was reported. In this paper, possibility of the terrestrial thin-film solar cell 's technologies for space applications is described. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047275005 |