{"created":"2023-06-20T15:17:13.230349+00:00","id":47371,"links":{},"metadata":{"_buckets":{"deposit":"da7bbcda-5966-43e0-936a-8be1a2e9c928"},"_deposit":{"created_by":1,"id":"47371","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"47371"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00047371","sets":["1887:1893","9:10:2065:2117"]},"author_link":["532516","532515","532520","532523","532517","532526","532519","532518","532525","532524","532522","532521","532527","532514"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Trade-Off Evaluation of the Integration Propulsion Systems for Space Explorations"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2021-02-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"19","bibliographicPageStart":"13","bibliographicVolumeNumber":"JAXA-RR-20-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告: 将来深宇宙探査に向けた革新的超小型推進系研究グループ 2020年度研究成果報告書"},{"bibliographic_title":"JAXA Research and Development Report: Technical Report of the Research Activity for Innovative Micro Propulsion Systems for Future Deep Space Explorations (2020)","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to obtain the exploration flexibility by the propulsion control technology of the micro-spacecraft, it is important to optimize the propulsion system. The objective of this paper is evaluated the trade-off of the chemical propulsion (CP) systems, the electric propulsion (EP) systems, and the combined CP and EP systems with shared propellant for 100 kg-class micro-spacecraft. As a result, it was confirmed that the effectiveness of combined CP and EP system with shared the high energetic propellant was clarified. In addition, at the higher thruster operation ratio for reaction control, it is necessary that the thruster performance is improved by using the higher thermal potential propellant. At the higher delta-V for orbit maneuver, it was confirmed that the integration propulsion systems of the higher thrust density are validity.","subitem_description_type":"Other"}]},"item_3_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_3_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_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA2030017003","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RR-20-008","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/00047358","subitem_identifier_reg_type":"JaLC"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2216","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS)"},{"subitem_text_value":"小山工業高等専門学校"},{"subitem_text_value":"東京都立大学"},{"subitem_text_value":"東京都立大学"},{"subitem_text_value":"宇宙航空研究開発機構研究開発部門第二研究ユニット(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所学際科学研究系(JAXA)(ISAS)"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"National Institute of Technology, Oyama College"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Research Unit II, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Department of Interdisciplinary Space Science, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_3_version_type_30":{"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":"和田, 明哲"}],"nameIdentifiers":[{"nameIdentifier":"532514","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"飯塚, 俊明"}],"nameIdentifiers":[{"nameIdentifier":"532515","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"佐原, 宏典"}],"nameIdentifiers":[{"nameIdentifier":"532516","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"各務, 聡"}],"nameIdentifiers":[{"nameIdentifier":"532517","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"渡邊, 裕樹"}],"nameIdentifiers":[{"nameIdentifier":"532518","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"船瀬, 龍"}],"nameIdentifiers":[{"nameIdentifier":"532519","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"羽生, 宏人"}],"nameIdentifiers":[{"nameIdentifier":"532520","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"WADA, 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