{"created":"2023-06-20T14:39:32.478499+00:00","id":6281,"links":{},"metadata":{"_buckets":{"deposit":"952f070b-3443-492b-984e-a70f73a5d70a"},"_deposit":{"created_by":1,"id":"6281","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6281"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006281","sets":["1887:1893","9:789:1031:1060"]},"author_link":["31657","31658","31656","31654","31659","31653","31655","31660"],"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 (FY16)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-01-20","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"128","bibliographicPageStart":"125","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":"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. We conducted the FMEA in order to investigate the method of lengthen the lifetime of 1N thruster. Then we found out these weak points: (1) Strength of catalyst bed metal mesh, and (2) Lifetime of catalyst granules. We conducted the material analysis of catalyst bed mesh wire that is removed from a life-tested thruster and firing test with the thruster imitation equipment.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049054025","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_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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"後藤, 大亮"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"香河, 英史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"増田, 井出夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"梶原, 堅一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Goto, Daisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kagawa, Hideshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masuda, Ideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kajiwara, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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","filename":"49054025.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49054025.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6281/files/49054025.pdf"},"version_id":"3f5f22e9-f188-45dc-8334-1c894057d68a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"ヒドラジン","subitem_subject_scheme":"Other"},{"subitem_subject":"1液推薬スラスタ","subitem_subject_scheme":"Other"},{"subitem_subject":"触媒","subitem_subject_scheme":"Other"},{"subitem_subject":"構造信頼性","subitem_subject_scheme":"Other"},{"subitem_subject":"金網","subitem_subject_scheme":"Other"},{"subitem_subject":"推薬分解","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hydrazine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"monopropellant thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"catalyst","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural reliability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wire mesh","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propellant decomposition","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":"衛星用1液スラスタの信頼性向上活動について(FY16)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"衛星用1液スラスタの信頼性向上活動について(FY16)"}]},"item_type_id":"3","owner":"1","path":["1060","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6281","relation_version_is_last":true,"title":["衛星用1液スラスタの信頼性向上活動について(FY16)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:58:35.091193+00:00"}