{"created":"2023-06-20T14:53:34.624846+00:00","id":21775,"links":{},"metadata":{"_buckets":{"deposit":"9ea35d14-1606-4be6-881a-7b1044329f25"},"_deposit":{"created_by":1,"id":"21775","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"21775"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00021775","sets":["1887:1888"]},"author_link":["204408","204409"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"World Trends in All-electric Satellite"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-09-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"9","bibliographicPageEnd":"279(21)","bibliographicPageStart":"274(16)","bibliographicVolumeNumber":"65","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会誌"},{"bibliographic_title":"Aeronautical and Space Sciences Japan","bibliographic_titleLang":"en"}]}]},"item_7_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"全電化静止衛星では推進系としてイオンエンジン, ホールスラスタ等の電気推進のみを搭載し, 軌道保持のみならず軌道上昇も電気推進にて行う. これにより従来の化学推進系に比して, 長い遷移期聞を要するものの大幅に搭載推薬量を削減することができる. 2015年, 米にて世界初の全電化静止衛星が打上げられ, イオンエンジンによる約半年間の軌道上昇後, 静止軌道に到達した．これに追従すべく, 各国で全電化静止衛星およびそれに搭載される電気推進の研究開発が活発化している．ホールスラスタはその高推力電力比により3～4カ月程度の短期間遷移を実現でき．さらに低コスト, ロバスト等の特徴も有し．全電化衛星向け電気推進の最有力候補とされる本稿では全電化静止衛星の世界動向を俯瞰するとともに, 全電化衛星への搭載が計画されているホールスラスタの開発動向についても概説する．","subitem_description_type":"Abstract"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: 図版あり","subitem_description_type":"Other"}]},"item_7_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: DS1740266003","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Japan Society for Aeronautical and Space Sciences"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0021-4663","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00189072","subitem_source_identifier_type":"NCID"}]},"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":"杵淵, 紀世志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kinefuchi, Kiyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"All-electric Satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Electric Propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hall Thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"全電化衛星の世界動向","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"全電化衛星の世界動向"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2017-09-22"},"publish_date":"2017-09-22","publish_status":"0","recid":"21775","relation_version_is_last":true,"title":["全電化衛星の世界動向"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:30:56.515693+00:00"}