{"created":"2023-06-19T10:28:47.857077+00:00","id":8346,"links":{},"metadata":{"_buckets":{"deposit":"59fa3352-edb1-4efd-a586-fd32a530f469"},"_deposit":{"created_by":18,"id":"8346","owners":[18],"pid":{"revision_id":0,"type":"depid","value":"8346"},"status":"published"},"_oai":{"id":"oai:muroran-it.repo.nii.ac.jp:00008346","sets":["216:290","35:175"]},"author_link":["489","52646","52647","52648","801","52644","52645","52658","52643"],"item_77_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2001-11-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"97","bibliographicPageStart":"91","bibliographicVolumeNumber":"51","bibliographic_titles":[{"bibliographic_title":"室蘭工業大学紀要","bibliographic_titleLang":"ja"},{"bibliographic_title":"Memoirs of the Muroran Institute of Technology","bibliographic_titleLang":"en"}]}]},"item_77_description_23":{"attribute_name":"フォーマット","attribute_value_mlt":[{"subitem_description":"application/pdf","subitem_description_type":"Other"}]},"item_77_description_7":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"Hybrid rocket motors, propelled by a combination of a solid fuel and a liquid oxidizer, are best suited to development of small launch systems in university laboratories, becauee af their advantageous characteristics such as Bafety, easy handling. and law costs. The performance of hybrid rocket motors of three classes of thrust - 10tonf, 1tonf, and 200kgf - is estimated. The feasibility of reusable winged launch systems based on the three motors is prelirninarily analyzed for suborbital micro-gravity experiments. The results tell that a sysbem with a 10tonf-class motor by a coolant bleed cycle with polystyrene and LOx fed by an LE-5B turbopump will be capabre of exposing a payload of 360kg to a micro-gravity environment for three minutes. It is also predictied that a system with a 1tonf-class motor will be moderately capable and that with a 200kgf-class motor will not be feasible for micro gravity missions mainly because the weight of its helium pressurization system for feeding LOx will reduce the mass fraction.","subitem_description_language":"en","subitem_description_type":"Abstract"}]},"item_77_description_8":{"attribute_name":"注記","attribute_value_mlt":[{"subitem_description":"小特集 : 「室蘭工大における航空宇宙工学研究の新展開」","subitem_description_language":"ja","subitem_description_type":"Other"}]},"item_77_link_5":{"attribute_name":"室蘭工業大学研究者データベースへのリンク","attribute_value_mlt":[{"subitem_link_text":"溝端 一秀（MIZOBATA Kazuhide）","subitem_link_url":"http://rdsoran.muroran-it.ac.jp/html/100000207_ja.html"}]},"item_77_publisher_11":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"室蘭工業大学","subitem_publisher_language":"ja"}]},"item_77_relation_15":{"attribute_name":"論文ID（NAID）","attribute_value_mlt":[{"subitem_relation_type":"isIdenticalTo","subitem_relation_type_id":{"subitem_relation_type_id_text":"110000076575","subitem_relation_type_select":"NAID"}}]},"item_77_rights_19":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"© 2001 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analysis","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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"再使用型有翼ハイブリットロケットシステムの基本設計と飛行性能予測","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"再使用型有翼ハイブリットロケットシステムの基本設計と飛行性能予測","subitem_title_language":"ja"},{"subitem_title":"Baseline Design and Flight Capability Predictions for a Reusable Winged Hybrid Rocket System","subitem_title_language":"en"}]},"item_type_id":"77","owner":"18","path":["175","290"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2007-06-06"},"publish_date":"2007-06-06","publish_status":"0","recid":"8346","relation_version_is_last":true,"title":["再使用型有翼ハイブリットロケットシステムの基本設計と飛行性能予測"],"weko_creator_id":"18","weko_shared_id":-1},"updated":"2023-12-22T03:13:58.401884+00:00"}