{"created":"2023-06-20T14:35:50.032714+00:00","id":2111,"links":{},"metadata":{"_buckets":{"deposit":"318d6866-e973-4191-a480-7289ef26bb66"},"_deposit":{"created_by":1,"id":"2111","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2111"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002111","sets":["1887:1893","9:10:132:142"]},"author_link":["3348","3340","3353","3345","3343","3349","3356","3351","3352","3339","3347","3355","3341","3346","3344","3354","3350","3342"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of a cold gas thruster for micro gravity experimental system with high altitude balloon"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03-31","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-08-005","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"現在JAXAでは，高々度気球からの自由落下を利用した微小重力実験装置の開発が進められている．この装置の特徴は，独特の二重殻構造を持つ点にあり，気球からの自由落下中に，内側の実験部を機体内部で浮遊させることで，30秒から60秒の良質な微小重力環境が得られる．落下中の機体姿勢制御，および実験部と機体内壁の隙間制御用に，合計16基の50N級コールドガスジェットスラスタが搭載されている．本稿では，微小重力実験装置用に開発されたガスジェットスラスタの設計と，その地上性能試験結果，飛行試験による実証結果について示す．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A novel method for micro-gravity experiments using high altitude balloon is now under development in JAXA. The notable feature of this system is its double-shell structure. Dropped from the high altitude balloon, the inner shell falls freely for 30 to 60 seconds because the outer shell is controlled not to collide with the inner shell. Sixteen number of cold gas thrusters are installed on the vehicle to control not only its falling attitude but also spacing between the inner shell and the outer shell. This paper presents design strategy and verification test results of the 50 N cold gas thrusters developed for this micro gravity experimental system. The preliminary results of the flight test are also presented to show its feasibility.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064328000","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-RR-08-005","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":"1349-1113","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":"AA1192675X","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研究開発本部ジェットエンジン技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙航行システム研究系"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙探査工学研究系"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙探査工学研究系"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙環境利用科学研究系"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙環境利用科学研究系"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部未踏技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙航行システム研究系"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙探査工学研究系"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Systems and Astronautics, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Spacecraft Engineering, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Spacecraft Engineering, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Biology and Microgravity Sciences, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Biology and Microgravity Sciences, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Systems and Astronautics, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Spacecraft Engineering, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小林, 弘明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"澤井, 秀次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"坂東, 信尚"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"坂井, 真一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 毅彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"稲富, 裕光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 和央"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"丸, 祐介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 樹明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sawai, Shujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Bando, Nobutaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakai, Shinichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Takehiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inatomi, Yuko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Kazuhisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maru, Yusuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Tatsuaki","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":"2020-01-15"}],"displaytype":"detail","filename":"64328000.pdf","filesize":[{"value":"6.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64328000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2111/files/64328000.pdf"},"version_id":"f962a6a2-08a1-4446-b6a4-3a9d0165a3c3"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Microgravity, Balloon, Drag-Free, Cold gas thruster","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":"気球利用型微少重力実験機用コールドガスジェットスラスタの開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"気球利用型微少重力実験機用コールドガスジェットスラスタの開発"}]},"item_type_id":"3","owner":"1","path":["142","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2111","relation_version_is_last":true,"title":["気球利用型微少重力実験機用コールドガスジェットスラスタの開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:28:27.264154+00:00"}