{"created":"2023-06-20T14:40:35.140117+00:00","id":7492,"links":{},"metadata":{"_buckets":{"deposit":"a6105d97-b049-4080-a431-814eff67fd33"},"_deposit":{"created_by":1,"id":"7492","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7492"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007492","sets":["1543:1544:1556","1887:1891"]},"author_link":["39968","39964","39962","39963","39970","39966","39967","39959","39965","39961","39960","39969"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"気球から自由落下する飛翔体における超音速飛行と引き起こし制御の検討"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"337","bibliographicPageStart":"333","bibliographic_titles":[{"bibliographic_title":"第17回アストロダイナミクスシンポジウム講演後刷り集　2007"},{"bibliographic_title":"Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"現在ISAS/JAXAでは気球を用いた微小重力実験装置の開発を進めている。この実験は、(1)高高度気球で高度40kmまで上昇させる、(2)実験機体を切り離す、(3)30-40秒間の自由落下を実現するものである。この実験において、落下機体は30秒程度落下したとき超音速になる。したがって、この実験機体は微小重力実験の他に簡易な超音速飛行試験を提供できると考えられる。実際に、空気吸い込み式エンジンを搭載しての実験も予定されている。この将来の実験において、エンジンの性能を測るために、十分な超音速飛行時間が必要です。そのため、高度40kmからの単純な落下では不十分であり、落下中機体を引き起こす必要がある。今回は、現行の機体で超音速飛行が実現できるかと、引き起こしによって超音速飛行時間を向上できるかを評価した幾つかのシミュレーション結果を示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The microgravity experimental system that uses the high altitude balloon is now developed in ISAS/JAXA. This experimental method is, (1) the high altitude balloon is raised to 40 km altitude, (2) the experimental system is separated, (3) a free fall for 30-40 seconds is achieved. In the experiment, the fall body enters a supersonic state when the free fall time exceeds about 30 seconds. Therefore, it can be expected that this fall body will offer a simple supersonic flight experiment besides the microgravity experiment. Actually, it is scheduled to equip the air inhalation type engine developing in the future. In this future experiment, an enough supersonic flight time is necessary to evaluate the performance of the engine. So it is thought that the nose of the body have to be put up since a simple fall from the altitude 40 km is insufficient. This paper evaluates whether a supersonic flight can be achieved in the present experimental system, and whether a supersonic time can be extended by putting the nose up. Some simulation results in several conditions are shown to verify the effectiveness of the putting the nose up of the experimental body.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063718055","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"武蔵工業大学"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"武蔵工業大学"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Musashi Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Musashi Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"門岡, 昇平"}],"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":"渡辺, 力夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 樹明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kadooka, Shohei","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":"Watanabe, Rikio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Tatsuaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"空気吸い込み式エンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"性能試験","subitem_subject_scheme":"Other"},{"subitem_subject":"制御系設計","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行経路","subitem_subject_scheme":"Other"},{"subitem_subject":"試験設備","subitem_subject_scheme":"Other"},{"subitem_subject":"高高度気球","subitem_subject_scheme":"Other"},{"subitem_subject":"自由落下","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"PD制御","subitem_subject_scheme":"Other"},{"subitem_subject":"迎角","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air breathing engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control system design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight path","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"test facility","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high altitude balloon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"free fall","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"PD control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Discussion about supersonic aviation and pullout control in free-fall flying object from balloon","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Discussion about supersonic aviation and pullout control in free-fall flying object from balloon","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1556","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7492","relation_version_is_last":true,"title":["Discussion about supersonic aviation and pullout control in free-fall flying object from balloon"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:40.727012+00:00"}