{"created":"2023-06-20T14:36:14.673270+00:00","id":2555,"links":{},"metadata":{"_buckets":{"deposit":"ff17b459-a931-44de-b73a-af873480899e"},"_deposit":{"created_by":1,"id":"2555","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2555"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002555","sets":["1887:1893","9:1090:1210:1211"]},"author_link":["7230","7235","7236","7237","7244","7245","7234","7231","7229","7239","7240","7242","7248","7233","7247","7232","7243","7246","7241","7238"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of Measurement Method of Roll Torque with Small Solid Rocket Motor"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011-03-31","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RM-10-019","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"これまでに実施された地上燃焼試験でのロールトルクの計測は，モータを横置きにした状態で実施され，燃焼中にロールトルクが発生し，燃焼室内で発生している燃焼ガスの旋回に起因していることを示唆する結果が得られたが，推進薬自重の変化が大きいことやロールトルクに対してモータ自重の影響が大きいことなどが原因で，詳細な評価が可能な計測レベルには達していない．そこで，本研究では，小型固体モータを用い，モータ自体を縦置きにした状態でエアベアリングを用い，押付方式および引張方式によるロールトルク計測実験を実施した．押付方式では，ロールトルクの発生は確認できたものの，その定量データは取得できなかった．一方，引張方式では精度は高くないがロールトルクの定量データが取得できた．得られたデータを過去の固体ロケットのロールトルクの特性と比較し，その値が妥当であることを確認し，エアベアリングを用いた引張方式によるロールトルク計測装置が，ロールトルクの計測に有効であることを確認した．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In previous study, results of measurements of roll torque at horizontal motor position in combustion ground tests showed that roll torque occurred during the combustion and it was caused by swirling flow of combustion gas generated in the solid rocket motor. However, because the shift of the propellant mass was large and the effect of weight of the motor was large, accuracy of measurement was not enough high to evaluate the roll torque minutely. In this study, the measurements of roll torque with a small solid rocket motor at vertical motor position by using an air bearing are conducted. Methods of measurements are measuring compressive loads or measuring tensile load. At the measuring compressive loads method, roll torque was confirmed, however, quantitative data of the roll torque was not obtained. On the other hand, at the measuring tensile load, the quantitative data of roll torque was obtained. The obtained data of the roll torque was compared with the characteristics of roll torque of other past solid rocket motors and it was confirmed that obtained data is proper value. This results shows that the new measurement system for roll torque is useful to measure roll torque of a solid rocket motor.","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: AA0064983000","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-RM-10-019","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11983593","subitem_source_identifier_type":"NCID"}]},"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輸送工学研究系"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所宇宙輸送工学研究系"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所宇宙科学技術・専門技術"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所観測ロケット実験室"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所基盤技術グループ"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所基盤技術グループ"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所推進系グループ"},{"subitem_text_value":"IHIエアロスペース・エンジニアリング開発部"},{"subitem_text_value":"IHIエアロスペース・エンジニアリング開発部"},{"subitem_text_value":"IHIエアロスペース・エンジニアリング開発部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Space Transportation Engineering, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Transportation Engineering, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Space Science and Disciplinary Engineering, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Sounding Rocket Laboratory, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Test and Operation Technology Group, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Test and Operation Technology Group, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Propulsion Group, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Development Department, IHI Aerospace Engineering"},{"subitem_text_language":"en","subitem_text_value":"Development Department, IHI Aerospace Engineering"},{"subitem_text_language":"en","subitem_text_value":"Development Department, IHI Aerospace Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"北川, 幸樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"嶋田, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安田, 誠一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉田, 裕二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"富澤, 利夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 直洋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加藤, 洋一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"尾澤, 剛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"二宮, 一芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"矢島, 卓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kitagawa, Koki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimada, Toru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yasuda, Seiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshida, Yuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tomizawa, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Naohiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Yoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ozawa, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ninomiya, Kazuyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yajima, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-15"}],"displaytype":"detail","filename":"64983000.pdf","filesize":[{"value":"2.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64983000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2555/files/64983000.pdf"},"version_id":"7f246e43-2b24-4c07-817d-0addfb486191"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Roll Torque","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Solid Rocket Motor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Ground Test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Measurement","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"小型固体モータを用いたロールトルク計測技術の開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型固体モータを用いたロールトルク計測技術の開発"}]},"item_type_id":"3","owner":"1","path":["1211","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2555","relation_version_is_last":true,"title":["小型固体モータを用いたロールトルク計測技術の開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:20:09.896146+00:00"}