WEKO3
アイテム
{"_buckets": {"deposit": "07d6d227-b09d-4281-a37f-02313bcfe242"}, "_deposit": {"created_by": 1, "id": "16796", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "16796"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00016796", "sets": ["1704", "1891"]}, "author_link": ["152757", "152755", "152751", "152758", "152756", "152754", "152753", "152752"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Performance measurement of electrothermal pulsed plasma thrusters for Osaka-Institute-of-Technology Electric-Rocket-Engine onboard Small Space Ship"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2009", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "5", "bibliographicPageStart": "1", "bibliographicVolumeNumber": "平成20年度", "bibliographic_titles": [{"bibliographic_title": "宇宙輸送シンポジウム: 講演集録"}, {"bibliographic_title": "Proceedings of Space Transportation Symposium", "bibliographic_titleLang": "en"}]}]}, "item_5_description_14": {"attribute_name": "会議概要(会議名, 開催地, 会期, 主催者等)", "attribute_value_mlt": [{"subitem_description": "平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部)", "subitem_description_type": "Other"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "The Project of Osaka-Institute-of-Technology Electric-Rocket-Engine onboard Small Space Ship (PROITERES) was started at Osaka Institute of Technology in 2007. In PROITERES, a 10-kg small satellite with electrothermal pulsed plasma thrusters (PPTs), named JOSHO, will be launched in 2010. The main mission is powered flight of small satellite by electric thruster itself. This study aims at improvement in performance by changing configuration of PPTs.The PPT with a discharge room diameter of 3.0 mm and an insulator length of 10.0 mm stably generated the highest impulse bit of 350 microNs.", "subitem_description_type": "Other"}]}, "item_5_description_18": {"attribute_name": "内容記述", "attribute_value_mlt": [{"subitem_description": "形態: カラー図版あり", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0064292103", "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)"}]}, "item_5_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AN10324301", "subitem_source_identifier_type": "NCID"}]}, "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: 013"}]}, "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": "大阪工業大学工学部"}, {"subitem_text_value": "大阪工業大学工学部"}, {"subitem_text_value": "大阪工業大学工学部"}, {"subitem_text_value": "大阪工業大学工学部"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Faculty of Engineering, Osaka Institute of Technology"}, {"subitem_text_language": "en", "subitem_text_value": "Faculty of Engineering, Osaka Institute of Technology"}, {"subitem_text_language": "en", "subitem_text_value": "Faculty of Engineering, Osaka Institute of Technology"}, {"subitem_text_language": "en", "subitem_text_value": "Faculty of Engineering, Osaka Institute of Technology"}]}, "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": "高木, 宏樹"}], "nameIdentifiers": [{"nameIdentifier": "152751", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "山本, 剛史"}], "nameIdentifiers": [{"nameIdentifier": "152752", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "石井, 悠介"}], "nameIdentifiers": [{"nameIdentifier": "152753", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "田原, 弘一"}], "nameIdentifiers": [{"nameIdentifier": "152754", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Takagi, Hiroki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "152755", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yamamoto, Tsuyoshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "152756", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ishii, Yusuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "152757", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Tahara, Hirokazu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "152758", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "PROITERES, Electric Propulsion, Pulsed Plasma Thruster, Small Satellite, Powered Flight", "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": "大阪工業大学・小型スペースシップ搭載用電熱加速型パルスプラズマスラスタの性能測定", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "大阪工業大学・小型スペースシップ搭載用電熱加速型パルスプラズマスラスタの性能測定"}]}, "item_type_id": "5", "owner": "1", "path": ["1704", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/16796", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "16796", "relation": {}, "relation_version_is_last": true, "title": ["大阪工業大学・小型スペースシップ搭載用電熱加速型パルスプラズマスラスタの性能測定"], "weko_shared_id": -1}
大阪工業大学・小型スペースシップ搭載用電熱加速型パルスプラズマスラスタの性能測定
https://jaxa.repo.nii.ac.jp/records/16796
https://jaxa.repo.nii.ac.jp/records/1679610fa8433-d390-4de0-bd57-a2533a983b3b
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 | 大阪工業大学・小型スペースシップ搭載用電熱加速型パルスプラズマスラスタの性能測定 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | PROITERES, Electric Propulsion, Pulsed Plasma Thruster, Small Satellite, Powered Flight | |||||
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 | Performance measurement of electrothermal pulsed plasma thrusters for Osaka-Institute-of-Technology Electric-Rocket-Engine onboard Small Space Ship | |||||
著者 |
高木, 宏樹
× 高木, 宏樹× 山本, 剛史× 石井, 悠介× 田原, 弘一× Takagi, Hiroki× Yamamoto, Tsuyoshi× Ishii, Yusuke× Tahara, Hirokazu |
|||||
著者所属 | ||||||
大阪工業大学工学部 | ||||||
著者所属 | ||||||
大阪工業大学工学部 | ||||||
著者所属 | ||||||
大阪工業大学工学部 | ||||||
著者所属 | ||||||
大阪工業大学工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Engineering, Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Engineering, Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Engineering, Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Engineering, Osaka Institute of Technology | ||||||
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) | |||||
書誌情報 |
宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium 巻 平成20年度, p. 1-5, 発行日 2009 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Project of Osaka-Institute-of-Technology Electric-Rocket-Engine onboard Small Space Ship (PROITERES) was started at Osaka Institute of Technology in 2007. In PROITERES, a 10-kg small satellite with electrothermal pulsed plasma thrusters (PPTs), named JOSHO, will be launched in 2010. The main mission is powered flight of small satellite by electric thruster itself. This study aims at improvement in performance by changing configuration of PPTs.The PPT with a discharge room diameter of 3.0 mm and an insulator length of 10.0 mm stably generated the highest impulse bit of 350 microNs. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324301 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064292103 |