{"created":"2023-06-20T14:49:36.706196+00:00","id":17500,"links":{},"metadata":{"_buckets":{"deposit":"bfde4f24-7896-4ac0-bc5a-f981c2ae649e"},"_deposit":{"created_by":1,"id":"17500","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"17500"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00017500","sets":["1543:1693:1711","1887:1891"]},"author_link":["158728","158730","158731","158724","158727","158726","158729","158725"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A solar thermal propulsion system for miniature satellites: A superminiature-scale solar thermal thrustor"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"292","bibliographicPageStart":"289","bibliographic_titles":[{"bibliographic_title":"宇宙輸送シンポジウム　平成13年度"},{"bibliographic_title":"Proceedings of Space Transportation Symposium FY2001","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本研究では外径5mm超々小型太陽熱スラスタの加熱実験の結果、および超小型衛星搭載時のコンポーネント案について報告した。(1)超々小型太陽熱スラスタの加熱試験(焦点位置:1cm)においてスラスタ外壁温度で1,379K、プレナム室温度で1,160Kを達成した。(2)超小型衛星衛星搭載時の太陽熱推進系のコンポーネント重量を見積もった結果、市販品で1.5kg以下となった。今後の課題として、高分子膜集光鏡との組み合わせによる加熱実験、焦点位置での加熱実験、単結晶モリブデン製スラスタでの加熱試験および噴射試験を行う。さらに本研究とこれらの課題の実験結果をもとに、超小型衛星に搭載して世界初の太陽熱推進系の宇宙実証試験を行いたい。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0033392072","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"法政大学 工学部"},{"subitem_text_value":"科学技術振興事業団"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"法政大学 工学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Hosei University Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Japan Science and Technology Corporation"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Hosei University Faculty of Engineering"}]},"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":"長, 慶太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐原, 宏典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 盛生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 嘉宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Osa, Keitaro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sahara, Hironori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimizu, Morio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Yoshihiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"太陽熱推進","subitem_subject_scheme":"Other"},{"subitem_subject":"イオン推進","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道変換機","subitem_subject_scheme":"Other"},{"subitem_subject":"熱効率","subitem_subject_scheme":"Other"},{"subitem_subject":"小型衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙環境","subitem_subject_scheme":"Other"},{"subitem_subject":"solar thermal propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ion propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit transfer vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal efficiency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"miniature satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace environment","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"超小型衛星用太陽熱推進系:超々小型太陽熱スラスタ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超小型衛星用太陽熱推進系:超々小型太陽熱スラスタ"}]},"item_type_id":"5","owner":"1","path":["1711","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"17500","relation_version_is_last":true,"title":["超小型衛星用太陽熱推進系:超々小型太陽熱スラスタ"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:37:18.171699+00:00"}