{"created":"2023-06-20T14:36:31.308622+00:00","id":2835,"links":{},"metadata":{"_buckets":{"deposit":"94f7a8af-ce27-4ad1-aa8d-4ed20db07d03"},"_deposit":{"created_by":1,"id":"2835","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2835"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002835","sets":["1398:1501:1502","1543:1827:1828","1887:1891","9:789:794:795"]},"author_link":["9182","9179","9175","9173","9172","9176","9178","9171","9180","9184","9174","9177","9185","9183","9170","9181"],"item_4_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Experimental Plan of Hypervelocity Impact Using Simulated SRM Slag"}]},"item_4_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2019-03-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"404","bibliographicPageStart":"383","bibliographicVolumeNumber":"JAXA-SP-18-011","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第8回スペースデブリワークショップ講演資料集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 8th Space Debris Workshop","bibliographic_titleLang":"en"}]}]},"item_4_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第8回スペースデブリワークショップ (2018年12月3-5日. 宇宙航空研究開発機構調布航空宇宙センター(JAXA)(CAC)), 調布市, 東京","subitem_description_type":"Other"}]},"item_4_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"The 8th Space Debris Workshop (December 3-5, 2018. Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)(CAC)), Chofu, Tokyo, Japan","subitem_description_type":"Other"}]},"item_4_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"アルミニウム粉を含む固体ロケットエンジンではノズル手前の淀み点近傍において、燃焼後アルミナが凝集される傾向があり、固体ロケットエンジン停止前後においてこの凝集されたアルミナの塊（SRM スラグ）が放出される可能性がある。一段目の固体ロケットエンジンは軌道速度に到達しないので大きな問題とはならないが、二段目以降で地球に対する周回軌道に入る場合、このSRM スラグも軌道速度を獲得し、スペースデブリとして周回する可能性がある。ISO24113の改定作業過程において、ヨーロッパを中心にSRMスラグに対する規制を強める方向で議論が進んだ。そこで、本研究ではSRM スラグが仮にスペースデブリとして周回軌道に入ってしまったとして、どの程度の危険性を有するのか、地上試験でSRMスラグを模擬した飛翔体を用意し、同じ大きさのアルミ球との比較を行う超高速衝突実験を立案することとした。本講演では、この実験計画ならびに予備実験について講演を行う予定である。","subitem_description_type":"Abstract"}]},"item_4_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Alumina particles trend to gather one another after combustion near stagnation point upper than nozzle of a solid rocket motor containing aluminum powder. Although there is no serious problem because the first solid rocket motor will not reach the earth orbit, SRM slag will reach the earth orbit and will go around the earth as space debris. In the process of revision of ISO24113, European P-members insisted to add regulation for SRM slag. So then in this we will study potential danger of SRM slag on space structures such as artificial satellites and so on if SRM slag goes around the earth orbit as space debris. Namely we will consider a plan of hypervelocity impact tests using a projectile which imitates SRM slag as well as aluminum sphere. In this presentation, we will address its experimental plan and some results of preliminary experiments.","subitem_description_type":"Other"}]},"item_4_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_4_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_4_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1830034031","subitem_description_type":"Other"}]},"item_4_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-18-011","subitem_description_type":"Other"}]},"item_4_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_4_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_4_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2232","subitem_source_identifier_type":"ISSN"}]},"item_4_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"九州工業大学"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"九州工業大学"},{"subitem_text_value":"九州工業大学"},{"subitem_text_value":"九州工業大学"},{"subitem_text_value":"九州工業大学"},{"subitem_text_value":"九州工業大学"},{"subitem_text_value":"九州工業大学"}]},"item_4_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"赤星, 保浩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"東出, 真澄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田上, 翔悟"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"池田, 仁哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉田, 冬威"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"花草, 孝史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"古賀, 想大"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高良, 隆男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Akahoshi, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Higashide, Masumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tagami, Shogo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ikeda, Masaya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshida, Toui","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hanakusa, Takafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koga, Sota","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koura, Takao","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":"AA1830034031.pdf","filesize":[{"value":"4.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1830034031.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2835/files/AA1830034031.pdf"},"version_id":"7928ed90-f94a-4e50-aaf4-8a5f38e1c80c"}]},"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":"conference object","resourceuri":"http://purl.org/coar/resource_type/c_c94f"}]},"item_title":"模擬SRM スラグ飛翔体を用いた超高速衝突実験計画","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"模擬SRM スラグ飛翔体を用いた超高速衝突実験計画"}]},"item_type_id":"4","owner":"1","path":["795","1502","1828","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2019-03-15"},"publish_date":"2019-03-15","publish_status":"0","recid":"2835","relation_version_is_last":true,"title":["模擬SRM スラグ飛翔体を用いた超高速衝突実験計画"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:15:19.745924+00:00"}