WEKO3
アイテム
{"_buckets": {"deposit": "98d7b474-c4a2-4bee-a9f7-5c4a5cbda545"}, "_deposit": {"created_by": 1, "id": "2727", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "2727"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00002727", "sets": ["1324", "1893"]}, "author_link": ["8611", "8612"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Development of heat transfer devices for thermal control of satellites"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-10-29", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "178", "bibliographicPageStart": "175", "bibliographicVolumeNumber": "JAXA-RM-04-010", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:衛星系"}, {"bibliographic_title": "JAXA Research and Development Memorandum: FY15 Annual Report of Research \u0026 Development on Space Technology in the Institute of Space Technology and Aeronautics: Satellite System", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Recently oscillating heat pipe (OHP) is desired for the thermal management system for future spacecraft. The principle of heat transfer of OHP is quite different from that of conventional heat pipe and its heat transfer ability is much higher than that of conventional one. To apply OHP to the spacecraft, the effect of gravity on the heat transfer of OHP should be examined. This paper describes the result of in-orbit experiment of micro-LabSat\u0027s onboard OHP.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0048057036", "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-RM-04-010", "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": "1349-1121", "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": "AA11983593", "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": "計装(計測制御装置の装備技術)及び写真技術"}, {"subitem_text_value": "流体力学及び熱伝導"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 研究開発資料"}]}, "item_3_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: RM"}]}, "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"}]}, "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"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "岡本, 篤"}], "nameIdentifiers": [{"nameIdentifier": "8611", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Okamoto, Atsushi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "8612", "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": "2020-01-15"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "48057036.pdf", "filesize": [{"value": "1.1 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1100000.0, "url": {"label": "48057036.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/2727/files/48057036.pdf"}, "version_id": "64752a64-81af-41aa-818b-47a125aa6851"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "ヒートパイプ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "温度制御", "subitem_subject_scheme": "Other"}, {"subitem_subject": "μ-LabSat", "subitem_subject_scheme": "Other"}, {"subitem_subject": "熱伝達", "subitem_subject_scheme": "Other"}, {"subitem_subject": "宇宙機設計", "subitem_subject_scheme": "Other"}, {"subitem_subject": "温度分布", "subitem_subject_scheme": "Other"}, {"subitem_subject": "温度センサ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ヒーター", "subitem_subject_scheme": "Other"}, {"subitem_subject": "heat pipe", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "temperature control", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "micro-LabSat", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "heat transfer", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "spacecraft design", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "temperature distribution", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "temperature sensor", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "heater", "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": "衛星搭載熱制御デバイスの開発実施状況", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "衛星搭載熱制御デバイスの開発実施状況"}]}, "item_type_id": "3", "owner": "1", "path": ["1324", "1893"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/2727", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "2727", "relation": {}, "relation_version_is_last": true, "title": ["衛星搭載熱制御デバイスの開発実施状況"], "weko_shared_id": -1}
衛星搭載熱制御デバイスの開発実施状況
https://jaxa.repo.nii.ac.jp/records/2727
https://jaxa.repo.nii.ac.jp/records/2727932c2b3f-188e-429e-bc78-9dcd678a7c3e
名前 / ファイル | ライセンス | アクション |
---|---|---|
48057036.pdf (1.1 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 | 衛星搭載熱制御デバイスの開発実施状況 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヒートパイプ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 温度制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | μ-LabSat | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝達 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 温度分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 温度センサ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヒーター | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat pipe | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | temperature control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | micro-LabSat | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat transfer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | temperature distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | temperature sensor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heater | |||||
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 | Development of heat transfer devices for thermal control of satellites | |||||
著者 |
岡本, 篤
× 岡本, 篤× Okamoto, Atsushi |
|||||
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 | ||||||
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研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:衛星系 en : JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Satellite System 巻 JAXA-RM-04-010, p. 175-178, 発行日 2004-10-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Recently oscillating heat pipe (OHP) is desired for the thermal management system for future spacecraft. The principle of heat transfer of OHP is quite different from that of conventional heat pipe and its heat transfer ability is much higher than that of conventional one. To apply OHP to the spacecraft, the effect of gravity on the heat transfer of OHP should be examined. This paper describes the result of in-orbit experiment of micro-LabSat's onboard OHP. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1121 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11983593 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0048057036 | |||||
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-RM-04-010 |