{"created":"2023-06-20T15:10:15.762337+00:00","id":39853,"links":{},"metadata":{"_buckets":{"deposit":"da17d521-2124-4ca5-9170-73303cd42c6d"},"_deposit":{"created_by":1,"id":"39853","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39853"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039853","sets":["1887:1893","1896:1898:1933:1934"]},"author_link":["500592","500595","500597","500599","500594","500589","500590","500593","500596","500588","500591","500598"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Experiment of passive damping system in airplane microgravity environment"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"34","bibliographicPageStart":"23","bibliographic_titles":[{"bibliographic_title":"宇宙開発事業団技術報告"},{"bibliographic_title":"NASDA Technical Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"NASDAは宇宙実験プログラムにおいて微小g-ジッタを低減するための制振システムの開発を進めている。受動制振システムは適用可能な幾つかの方法の1つである。微小重力環境を模擬した地上実験を経て開発した制振継手およびアイソレータを用いて受動制振システムの実験装置を試作した。1990年9月に第1回の航空機実験を実施し、実際の微小重力環境下での受動制振システムの機能を評価した。制振継手を用いた制振ラックが微小振動を増幅する効果を持つ共振倍率を1/2〜1/4に低減させたこと、およびアイソレータが0.1Hzの低周波数からの振動を遮断したことを確認した。第1回の実験結果に基づき、航空機の微小重力に適合するようにアイソレータの形状および剛性を再設計した。1991年12月から1992年1月にかけて、第2回の航空機実験を実施した。本論文では第2回の実験結果を述べた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"NASDA is developing a damping system for the reduction of micro g-jitter in the space experiment programs. A passive damping system is one of several applicable methods. The engineering model for passive damping system has been made using damping joints and isolators which had been developed through ground experiments simulating microgravity environment. The first airplane experiment was conducted in September, 1990, and the function of passive damping system was evaluated under the actual microgravity environment. It was confirmed that the damping rack, using damping joint, reduced the resonance magnification which had the effect of amplifying microvibration to 1/2-1/4, and that the isolator isolated vibration from low frequency of 0.1 Hz. Based on the first experimental result, the shape and rigidity of isolator were redesigned to fit the microgravity of airplane. In the period from December 1991 to January 1992, the second airplane experiment was conducted. This paper describes the results of the second airplane experiment.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000740003","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: NASDA-TMR-960023","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙開発事業団"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Space Development Agency of Japan (NASDA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1345-7888","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":"AN00364784","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"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙環境利用推進センター"},{"subitem_text_value":"日本電気"},{"subitem_text_value":"日本電気航空宇宙システム"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"Japan Space Utilization Promotion Center"},{"subitem_text_language":"en","subitem_text_value":"NEC Corporation"},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"清水, 盛生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"楠瀬, 智宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加藤, 充康"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石倉, 精三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"留目, 一英"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉永, 秀明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimizu, Morio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kusunose, Tomohiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Mitsuyasu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikura, Seizo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Todome, Kazuhide","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshinaga, Hideaki","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":"2020-02-10"}],"displaytype":"detail","filename":"00740003.pdf","filesize":[{"value":"784.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"00740003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39853/files/00740003.pdf"},"version_id":"0b495b31-71f8-4d00-a249-dc5186b01fdc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"MU-300型航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"パラボリックフライト","subitem_subject_scheme":"Other"},{"subitem_subject":"微小重力環境","subitem_subject_scheme":"Other"},{"subitem_subject":"受動制振システム","subitem_subject_scheme":"Other"},{"subitem_subject":"微小g-ジッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"制振継手","subitem_subject_scheme":"Other"},{"subitem_subject":"共鳴倍率","subitem_subject_scheme":"Other"},{"subitem_subject":"制振ラック","subitem_subject_scheme":"Other"},{"subitem_subject":"微小振動","subitem_subject_scheme":"Other"},{"subitem_subject":"アイソレータ","subitem_subject_scheme":"Other"},{"subitem_subject":"振動低減","subitem_subject_scheme":"Other"},{"subitem_subject":"ペイロードクランプ","subitem_subject_scheme":"Other"},{"subitem_subject":"MU 300 aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parabolic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microgravity environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"passive damping system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"micro g jitter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"damping joint","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"resonance magnification","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"damping rack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microvibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"isolator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"payload clamp","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":"航空機の微小重力環境下における受動制振システム実験装置評価実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空機の微小重力環境下における受動制振システム実験装置評価実験"}]},"item_type_id":"3","owner":"1","path":["1893","1934"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39853","relation_version_is_last":true,"title":["航空機の微小重力環境下における受動制振システム実験装置評価実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T20:28:47.685284+00:00"}