{"created":"2023-06-20T15:03:09.849763+00:00","id":32291,"links":{},"metadata":{"_buckets":{"deposit":"2ab2240b-a936-4615-9de0-2c0411be22cc"},"_deposit":{"created_by":1,"id":"32291","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32291"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032291","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["408166","408159","408162","408167","408165","408164","408161","408168","408163","408160"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Observation of Near-Infrared Airglow and the Determination of the Rocket Atitude"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1972-03","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1_B","bibliographicPageEnd":"68","bibliographicPageStart":"59","bibliographicVolumeNumber":"8","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"赤外黄道光の観測を目的としたK-10-4号機による実験の結果,強い近赤外大気光が観測された.東西の地平線方向に現われる大気大の強度を時間の関数として表わすと,ロケットのスピン周期,プレセッションの半総角と周丿匪 およびロケット軸の天頂角が求められる.本稿に述べる方法は,地平線センサを用いてロケットの姿勢を決める一般論となる.この方法を利用して赤外望遠鏡の視線の向きが決められる.視線が発光層を過ぎる点が得られ,その点における日没後の時間が求まる.これから夜光強度の日没後の時間的変化が得られる.O_2(^1&litri;_g-3Σ√_g^-)(0,0)帯の1.27μの強度の減衰率がこうして求められた.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Airglow in the near infrared range (λλ 1. 1-2.4μ) was observed by a sounding rocket K-10-4. The rocket roll angle between two intensity maxima due to airglow was found to change as the rocket altitude increased. This allows us to determine the zenith angle of the rocket axis and the height of the air glow layer. The roll angle for the airglow peak wiggled according to the precession of the rocket. The zenith angle of the precession axis and the cone half angle of the precession were thus determined to be 29°±1° and 1.5°, respectively. The heights at the maximum airglow emission were obtained as 72 km for the J band (1.27μ) and 77km for the K-band (2.2μ). Owing to the precession, the airglow emissions at varying local times were obtained. The half-life of an excited state of O_2 emitting 1.27μ, line was obtained to be 30min. This is compared with its half-life of 42 min. for the spontaneous decay.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125467000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"名古屋大学理学部"},{"subitem_text_value":"名古屋大学理学部"},{"subitem_text_value":"名古屋大学理学部"},{"subitem_text_value":"名古屋大学理学部"},{"subitem_text_value":"名古屋大学理学部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"早川, 幸男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 浩弐"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松本, 敏雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西村, 徹郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野, 忠良"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HAYAKAWA, Satio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ITOH, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MATSUMOTO, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NISHIMURA, Tetsuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ONO, Tadayoshi","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0125467.pdf","filesize":[{"value":"492.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125467.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32291/files/SA0125467.pdf"},"version_id":"8d8e3ab3-6cb2-4e89-8f2f-4e5d6c72dc4e"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"近赤外夜光の観測とロケットの姿勢決定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"近赤外夜光の観測とロケットの姿勢決定"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32291","relation_version_is_last":true,"title":["近赤外夜光の観測とロケットの姿勢決定"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:36:19.605039+00:00"}