{"created":"2023-06-20T15:10:04.666499+00:00","id":39671,"links":{},"metadata":{"_buckets":{"deposit":"0ee74335-850b-4493-a4c5-a791c68319b9"},"_deposit":{"created_by":1,"id":"39671","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39671"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039671","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["443807","443806"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Design and fabrication of an ion thruster thrust test stand"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"13","bibliographicPageStart":"1","bibliographicVolumeNumber":"669","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"イオンエンジン推力を直接測定する推力試験装置を設計し、製作した。この試験装置の機能確認のため、較正試験と14cmカスプ型キセノンイオンエンジンを用いて、直接推力測定を行った。製作した推力試験装置は振子型で、推力は振子の変位量から求める。推力と変位量の関係を求めるため、精密に計測した分銅を用いて、較正試験を行った。その結果、この装置は、良い比例関係を持つことが確かめられた。イオンエンジン推力を直接測定する時、エンジン作動に必要な電力・推進剤の供給は、配線・配管のそれぞれで行った。これらは振子と同様に動く。そのため、これらの変位量への影響について調べた。その結果、影響は予想以上に大きいことが分かった。本報告書は、この装置の機能を解説するとともに、この装置が推力測定のために十分な能力を持っているか試験し、その結果について述べる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A thrust test stand to measure the thrust of an ion thruster was designed and manufactured. The stand was calibrated and the thrust of a 14-cm diameter xenon ion thruster was measured. The stand was composed of a rigid pendulum and knife edges. The thruster was held by the pendulum and the thrust was gauged by the displacement of the pendulum. Propellant-feed piping and electrical cables were connected to the thruster and their stiffness reduced the displacement. The displacement, however, was still found to be linearly dependent on the thrust. This study presents the minutia of the stand and the calibration, and the results of thrust measurement.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000091000","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: NAL TM-669","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 宇宙研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Space Technology Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"宮崎, 勝弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazaki, Katsuhiro","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm00669.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00669.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39671/files/naltm00669.pdf"},"version_id":"0d334a55-6679-4079-ae14-2b14f99e7d07"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"イオンエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"推力試験装置","subitem_subject_scheme":"Other"},{"subitem_subject":"システム設計","subitem_subject_scheme":"Other"},{"subitem_subject":"キセノン推進剤","subitem_subject_scheme":"Other"},{"subitem_subject":"比推力","subitem_subject_scheme":"Other"},{"subitem_subject":"推力測定装置","subitem_subject_scheme":"Other"},{"subitem_subject":"振子型装置","subitem_subject_scheme":"Other"},{"subitem_subject":"ナイフエッジ機構","subitem_subject_scheme":"Other"},{"subitem_subject":"推力検出器","subitem_subject_scheme":"Other"},{"subitem_subject":"ダンピング装置","subitem_subject_scheme":"Other"},{"subitem_subject":"較正試験","subitem_subject_scheme":"Other"},{"subitem_subject":"ビームプラズマ放電","subitem_subject_scheme":"Other"},{"subitem_subject":"性能評価","subitem_subject_scheme":"Other"},{"subitem_subject":"ion thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust test stand","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"system design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"xenon propellant","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"specific thrust","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust measurement instrument","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pendulum type device","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"knife edge motion mechanism","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust detector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"damper","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"beam plasma discharge","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"evaluation of performance","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":"イオンエンジン推力試験装置の設計と製作","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"イオンエンジン推力試験装置の設計と製作"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39671","relation_version_is_last":true,"title":["イオンエンジン推力試験装置の設計と製作"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:57.644301+00:00"}