WEKO3
アイテム
{"_buckets": {"deposit": "c3db0636-91d5-4a0a-9691-7aaa8f2643fb"}, "_deposit": {"created_by": 1, "id": "2724", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "2724"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00002724", "sets": ["1324", "1893"]}, "author_link": ["8602", "8599", "8601", "8600", "8597", "8598"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Reliability improvement of catalytic monopropellant thrusters"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-10-29", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "164", "bibliographicPageStart": "159", "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": "Catalytic monopropellant thrusters have been loaded in many satellites for reaction control system, because of the reliable simple structure and about 200 sec moderate specific impulse. Nowadays, satellites mass and lifetimes have been increasing, however, Japanese monopropellant thrusters designs were not improved basically. It is therefore thrusters lifetimes have little margin for satellite demand especially in the 1N thruster. During qualification firing test, some malfunctions (ex. misfiring) occurred. Activities for improving thruster reliability have been conducted since FY2000. The results of FY2003 are presented here.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0048057033", "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": "宇宙船の推進及び出力"}, {"subitem_text_value": "推進剤及び燃料"}]}, "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"}, {"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"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "後藤, 大亮"}], "nameIdentifiers": [{"nameIdentifier": "8597", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "香河, 英史"}], "nameIdentifiers": [{"nameIdentifier": "8598", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "梶原, 堅一"}], "nameIdentifiers": [{"nameIdentifier": "8599", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Goto, Daisuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "8600", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kagawa, Hideshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "8601", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kajiwara, Kenichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "8602", "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": "48057033.pdf", "filesize": [{"value": "1.6 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1600000.0, "url": {"label": "48057033.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/2724/files/48057033.pdf"}, "version_id": "fb973caf-678b-4a16-9940-4db9a0a22c9d"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "信頼性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "触媒モノプロペラントスラスタ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "パルスモードスラスタ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "反応制御", "subitem_subject_scheme": "Other"}, {"subitem_subject": "比推力", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ヒドラジン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "可視化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "点火試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "reliability", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "catalytic monopropellant thruster", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "pulse mode thruster", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "reaction control", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "specific impulse", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "hydrazine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "visualization", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "firing test", "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": "触媒スラスタの信頼性向上", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "触媒スラスタの信頼性向上"}]}, "item_type_id": "3", "owner": "1", "path": ["1324", "1893"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/2724", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "2724", "relation": {}, "relation_version_is_last": true, "title": ["触媒スラスタの信頼性向上"], "weko_shared_id": -1}
触媒スラスタの信頼性向上
https://jaxa.repo.nii.ac.jp/records/2724
https://jaxa.repo.nii.ac.jp/records/27241aee3e08-33bc-4c0d-983f-25909167720d
名前 / ファイル | ライセンス | アクション |
---|---|---|
48057033.pdf (1.6 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 | 触媒スラスタの信頼性向上 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 信頼性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 触媒モノプロペラントスラスタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | パルスモードスラスタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 反応制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 比推力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヒドラジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 可視化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 点火試験 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reliability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | catalytic monopropellant thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pulse mode thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reaction control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | specific impulse | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hydrazine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | visualization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | firing test | |||||
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 | Reliability improvement of catalytic monopropellant thrusters | |||||
著者 |
後藤, 大亮
× 後藤, 大亮× 香河, 英史× 梶原, 堅一× Goto, Daisuke× Kagawa, Hideshi× Kajiwara, Kenichi |
|||||
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 | ||||||
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. 159-164, 発行日 2004-10-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Catalytic monopropellant thrusters have been loaded in many satellites for reaction control system, because of the reliable simple structure and about 200 sec moderate specific impulse. Nowadays, satellites mass and lifetimes have been increasing, however, Japanese monopropellant thrusters designs were not improved basically. It is therefore thrusters lifetimes have little margin for satellite demand especially in the 1N thruster. During qualification firing test, some malfunctions (ex. misfiring) occurred. Activities for improving thruster reliability have been conducted since FY2000. The results of FY2003 are presented here. | |||||
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: AA0048057033 | |||||
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 |