{"created":"2023-05-15T11:59:33.047113+00:00","id":6024,"links":{},"metadata":{"_buckets":{"deposit":"ede36dba-3d8c-4f25-a75f-63300377a28d"},"_deposit":{"created_by":3,"id":"6024","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"6024"},"status":"published"},"_oai":{"id":"oai:kyutech.repo.nii.ac.jp:00006024","sets":["15:20"]},"author_link":["24677","24678","24676","5459","24675"],"item_23_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2015-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"278","bibliographicPageStart":"273","bibliographicVolumeNumber":"103","bibliographic_titles":[{"bibliographic_title":"Procedia Engineering"}]}]},"item_23_description_4":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"For assessing the NEO orbit change by spacecraft impact, it is necessary to clarify the momentum shift at the impact time. Momentum shift is various amounts depending on the material of projectile and target, their shapes, and impact velocity. Currently, we have to collect more impact data by performing a simulated impact test on the earth because we do not have enough data to discuss design of a spacecraft impacter. Generally speaking, momentum shift is described at β (= about 1 ∼ 10 in other institution's impact tests). We aim to get more efficient momentum shift by creating experimental conditions in which β is larger than 10. In this study, we developed a test equipment of pendulum type for measuring β, and performed impact tests after calibration of the pendulum equipment.","subitem_description_type":"Abstract"}]},"item_23_description_5":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"2015 Hypervelocity Impact Symposium (HVIS 2015), April 27-30, 2015, Boulder, Colorado","subitem_description_type":"Other"}]},"item_23_description_60":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"subitem_description":"Conference Paper","subitem_description_type":"Other"}]},"item_23_publisher_7":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Elsevier"}]},"item_23_relation_12":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_type":"isIdenticalTo","subitem_relation_type_id":{"subitem_relation_type_id_text":"https://doi.org/10.1016/j.proeng.2015.04.047","subitem_relation_type_select":"DOI"}}]},"item_23_rights_13":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"Copyright (c) 2015 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)."}]},"item_23_select_59":{"attribute_name":"査読の有無","attribute_value_mlt":[{"subitem_select_item":"yes"}]},"item_23_source_id_8":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1877-7058","subitem_source_identifier_type":"ISSN"}]},"item_23_text_37":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan"},{"subitem_text_value":"Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan"},{"subitem_text_value":"Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan"},{"subitem_text_value":"Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan"},{"subitem_text_value":"Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan"}]},"item_23_text_62":{"attribute_name":"連携ID","attribute_value_mlt":[{"subitem_text_value":"7704"}]},"item_23_version_type_58":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Kage,  Shohei"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uenishi,  Satoshi"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka,  Masashi"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koura,  Takao"}],"nameIdentifiers":[{}]},{"creatorAffiliations":[{"affiliationNameIdentifiers":[],"affiliationNames":[{"affiliationName":"","affiliationNameLang":"ja"}]}],"creatorNames":[{"creatorName":"Akahoshi, Yasuhiro","creatorNameLang":"en"},{"creatorName":"赤星, 保浩","creatorNameLang":"ja"},{"creatorName":"アカホシ, ヤスヒロ","creatorNameLang":"ja-Kana"}],"familyNames":[{},{},{}],"givenNames":[{},{},{}],"nameIdentifiers":[{},{},{},{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2019-06-20"}],"displaytype":"detail","filename":"LaSEINE-2015_17.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"LaSEINE-2015_17.pdf","url":"https://kyutech.repo.nii.ac.jp/record/6024/files/LaSEINE-2015_17.pdf"},"version_id":"c4e5afad-b129-44fc-b370-1c1fe8649ce4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Hypervelocity impact","subitem_subject_scheme":"Other"},{"subitem_subject":"momentum shift","subitem_subject_scheme":"Other"},{"subitem_subject":"space guard","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":"Development of Equipment to Estimate Momentum Shift in NEO Orbit Change by a Spacecraft Impact","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Development of Equipment to Estimate Momentum Shift in NEO Orbit Change by a Spacecraft Impact"}]},"item_type_id":"23","owner":"3","path":["20"],"pubdate":{"attribute_name":"公開日","attribute_value":"2019-06-20"},"publish_date":"2019-06-20","publish_status":"0","recid":"6024","relation_version_is_last":true,"title":["Development of Equipment to Estimate Momentum Shift in NEO Orbit Change by a Spacecraft Impact"],"weko_creator_id":"3","weko_shared_id":3},"updated":"2023-10-25T08:21:08.298606+00:00"}