{"created":"2023-06-20T14:39:18.649356+00:00","id":6046,"links":{},"metadata":{"_buckets":{"deposit":"9efe8907-2b7b-42b1-b810-f78e0e7b4465"},"_deposit":{"created_by":1,"id":"6046","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6046"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006046","sets":["1887:1893","9:789:998:1028"]},"author_link":["30118","30119","30115","30120","30116","30117"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The development of a Japanese 20N thruster valve for a spacecraft propulsion system"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-11-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"290","bibliographicPageStart":"285","bibliographicVolumeNumber":"JAXA-SP-06-006","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書"},{"bibliographic_title":"JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Japan Aerospace Exploration Agency (JAXA) is now developing a 20N-class thruster valve for spacecraft propulsion systems. We intend to develop this valve with the high reliability, and a robust and durable design. The suspended armature type was chosen for the base design of the new 20N valve based on the results of a trade-off study. Experiments and analysis were performed for the critical parts and manufacturing process. The results enabled us to manufacture a prototype model with single type 20N thruster valves. Good results were obtained in functional tests. We will now proceed to the next phase and complete the detailed design for series redundancy and prepare for the qualification test.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049500062","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-06-006","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"}]},"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 Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"長田, 泰一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"櫛木, 賢一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"梶原, 堅一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagata, Taiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kushiki, Kenichi","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":"49500062.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49500062.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6046/files/49500062.pdf"},"version_id":"e964ab79-9ec6-4561-bb49-0d4a3bb803d9"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"推薬弁","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機推進","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機マヌーバ","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"ソレノイド弁","subitem_subject_scheme":"Other"},{"subitem_subject":"冗長部品","subitem_subject_scheme":"Other"},{"subitem_subject":"冗長性","subitem_subject_scheme":"Other"},{"subitem_subject":"応力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"振動試験","subitem_subject_scheme":"Other"},{"subitem_subject":"共鳴周波数","subitem_subject_scheme":"Other"},{"subitem_subject":"thruster valve","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft maneuver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solenoid valve","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"redundant component","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"redundancy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stress distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"resonant frequency","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":"人工衛星用20N推薬弁の国産開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"人工衛星用20N推薬弁の国産開発"}]},"item_type_id":"3","owner":"1","path":["1028","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6046","relation_version_is_last":true,"title":["人工衛星用20N推薬弁の国産開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:03:18.204131+00:00"}