{"created":"2023-05-15T11:59:34.882370+00:00","id":6068,"links":{},"metadata":{"_buckets":{"deposit":"2e1744b9-a358-465f-8219-b016d4319e10"},"_deposit":{"created_by":3,"id":"6068","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"6068"},"status":"published"},"_oai":{"id":"oai:kyutech.repo.nii.ac.jp:00006068","sets":["15:20"]},"author_link":["24904","24905","5459","24902","24903"],"item_23_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"145","bibliographicPageStart":"138","bibliographicVolumeNumber":"204","bibliographic_titles":[{"bibliographic_title":"Procedia Engineering"}]}]},"item_23_description_4":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"NEO (Near Earth Object) are the celestial bodies which pass near the Earth. One NEO deflection method is spacecraft impact. In order to estimate its results, it is necessary to clarify mechanism of momentum change of NEO. Generally, β is used as an evaluation index in this field and affected by various factors, so this study focuses on spacecraft shape. Five types of projectile shape were tested and compared in term of two aspects. In addition, we made comparison by using scaling law in order to compare the shape effect in the speed region which is assumed to using actual NEO deflection.","subitem_description_type":"Abstract"}]},"item_23_description_5":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"14th Hypervelocity Impact Symposium 2017(HVIS2017), 24-28 April 2017, Canterbury, Kent, UK","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.2017.09.766","subitem_relation_type_select":"DOI"}}]},"item_23_rights_13":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"Copyright (c) 2017 The Authors. Published by Elsevier Ltd."}]},"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":"7716"}]},"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":"Ikeda,  Masaya"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka,  Masashi"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yokoo,  Daisuke"}],"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":"2019-07-04"}],"displaytype":"detail","filename":"LaSEINE-2017_12.pdf","filesize":[{"value":"665.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"LaSEINE-2017_12.pdf","url":"https://kyutech.repo.nii.ac.jp/record/6068/files/LaSEINE-2017_12.pdf"},"version_id":"83a533ff-25ec-4650-af60-50222bedcfaa"}]},"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":"Study of the Effects of Projectile Shape in the Asteroid Orbit Change by Spacecraft Impact","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Study of the Effects of Projectile Shape in the Asteroid Orbit Change by Spacecraft Impact"}]},"item_type_id":"23","owner":"3","path":["20"],"pubdate":{"attribute_name":"公開日","attribute_value":"2019-07-04"},"publish_date":"2019-07-04","publish_status":"0","recid":"6068","relation_version_is_last":true,"title":["Study of the Effects of Projectile Shape in the Asteroid Orbit Change by Spacecraft Impact"],"weko_creator_id":"3","weko_shared_id":3},"updated":"2023-10-25T08:21:07.861598+00:00"}