{"created":"2023-06-20T14:40:43.901488+00:00","id":7655,"links":{},"metadata":{"_buckets":{"deposit":"e27735bf-0956-4259-b3f3-ade32f23e681"},"_deposit":{"created_by":1,"id":"7655","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7655"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007655","sets":["1543:1544:1559","1887:1891"]},"author_link":["41015","41019","41018","41013","41017","41016","41014","41020"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"M-Vロケット6号機サブペイロードを利用した超小型衛星用分離機構の軌道上実験システム"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"126","bibliographicPageStart":"121","bibliographic_titles":[{"bibliographic_title":"平成16年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本研究では、超小型衛星用分離機構の汎用化を目指し、M-Vロケット6号機のサブペイロードを用いて分離実証実験を行うべく準備を進めている。300mm×150mm×125mmの空間内に、分離機構、ダミー衛星、計測装置、電源制御、通信、分離許可信号処理システムなどを搭載し、打ち上げ1,421秒後から168秒間、クリスマス島可視領域において実験を行う。本稿では、実験の概要、開発状況、評価のための解析項目などについて述べる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Laboratory for Space Systems (LSS) prepares an on-orbit experiment of a separation mechanism for nano-satellite on a sub-payload of M-V Rocket No.6. The sub-payload is a space for a counter weight to motion balance of the M-V rocket. LSS was permitted to use the space to conduct the present experiments. The size of the sub-payload is about 300 mm x 150 mm x 124 mm. The weight is 5 kg, provided that the allowable margin of error is less than 5 percent. The experiment system consists of the separation mechanism, a dummy mass instead of a pico-satellite, a measurement subsystem and a rocket interface subsystem. The dummy mass is a substitute for a pico-satellite. The size is 10 cm cubic and weight is about 1 kg. The measurement subsystem measures a separation speed, a motion of the dummy mass after separation and temperatures at four points. The rocket interface subsystem consists of a power, communication and timer receiving. The system attached B3PL of M-V rocket turns on before the launch and conducts a separation after 1,421 s from the launch. Acquired data in the separation are transmitted for 168 s at Christmas Island in the Republic of Kiribati. The paper describes overview, development status and measurement item to verify the system.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897022","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and 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":"宇井, 恭一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮下, 直己"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮本, 径"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松永, 三郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ui, Kyoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyashita, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyamoto, Kei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsunaga, Saburo","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超小型衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"分離機構","subitem_subject_scheme":"Other"},{"subitem_subject":"分離速度","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道上実験システム","subitem_subject_scheme":"Other"},{"subitem_subject":"光電センサー","subitem_subject_scheme":"Other"},{"subitem_subject":"熱解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"実験","subitem_subject_scheme":"Other"},{"subitem_subject":"pico-satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"separation mechanism","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"separation speed","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"on-orbit experiment system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"photoelectric sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"experimentation","subitem_subject_language":"en","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":"On-orbit experiment system of separation mechanism for pico-satellite on sub-payload of M-V rocket","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"On-orbit experiment system of separation mechanism for pico-satellite on sub-payload of M-V rocket","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1559","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7655","relation_version_is_last":true,"title":["On-orbit experiment system of separation mechanism for pico-satellite on sub-payload of M-V rocket"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:07.995649+00:00"}