{"created":"2023-06-20T15:10:12.588831+00:00","id":39804,"links":{},"metadata":{"_buckets":{"deposit":"9c7b6058-f782-48d7-95ea-ca3005278386"},"_deposit":{"created_by":1,"id":"39804","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39804"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039804","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["522141","522140","444534","444536"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research on reliability criteria of upper stage solid rocket motors. Part 3: Firing test of scaled motors with various defects"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-06","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"62","bibliographicPageStart":"1","bibliographicVolumeNumber":"1298","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"国産・自主技術で進めたH-1ロケット用第3段モータおよびアポジ・モータの開発において重要な要素である信頼性の確立を図るため、航空宇宙技術研究所(NAL)と宇宙開発事業団(NASDA)が研究グループ「上段固体モータ信頼性研究グループ」を結成し、共同研究「上段固体ロケットモータの信頼性評価基準に関する実験的研究」を1980年度から1984年度まで行った。そしてその主体である推進薬の欠陥許容判定基準の研究および推進薬の欠陥検出法の研究についての成果をその後の研究成果も含めて3部作の報告書にまとめた。なお、本共同研究はNAL特別研究「上段モータの信頼性評価基準に関する研究」と緊密な関係のもとで行われた。本報告書では、国産開発のH-1アポジ・モータの1/4縮尺モータなどの小型モータに、推進薬気泡、インシュレーション・推進薬間剥離、推進薬ノッチなどの人工欠陥を付し、欠陥の燃焼への影響を調べた結果について述べる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to establish high reliability of the first domestically developed apogee and third motors of the H-1 rocket, NAL and NASDA performed coresearch of 'Experimental Research on Reliability Criteria of the Upper Stage Solid Rocket Motors', by organizing 'Upper Stage Solid Motor Reliability Research Group' for 1980 to 1984. The research consisted of 'Investigation on Tolerance Criteria of Solid Propellant Defects' and 'Nondestructive Inspection Method of Propellant Defects', and much data was collected in these studies, being supported by NAL special research activities. This third report presents combustion results of 1/4 scaled motors of the H-1 apogee motor with various defects such as bubbles, case/liner and liner/propellant separations, and propellant notch and crack under X ray TV observation, and the relation between the defects and the combustion properties was determined.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000592000","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: NAL TR-1298","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"航空宇宙技術研究所 宇宙研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Space Technology Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"上段固体モータ信頼性研究グループ"}],"nameIdentifiers":[{"nameIdentifier":"444534","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"上段固体モータ信頼性研究グループ"}],"nameIdentifiers":[{"nameIdentifier":"522140","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Upper Stage Solid Motor Reliability Research Group","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"444536","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Upper Stage Solid Motor Reliability Research Group","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"522141","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-27"}],"displaytype":"detail","filename":"naltr01298.pdf","filesize":[{"value":"25.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01298.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39804/files/naltr01298.pdf"},"version_id":"a4a5df67-f448-4761-8381-91ff31be9f5a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"信頼性評価基準","subitem_subject_scheme":"Other"},{"subitem_subject":"固体ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"上段固体モータ","subitem_subject_scheme":"Other"},{"subitem_subject":"H-1アポジモータ","subitem_subject_scheme":"Other"},{"subitem_subject":"縮尺モータ","subitem_subject_scheme":"Other"},{"subitem_subject":"人工欠陥","subitem_subject_scheme":"Other"},{"subitem_subject":"推進薬ノッチ","subitem_subject_scheme":"Other"},{"subitem_subject":"推進薬気泡","subitem_subject_scheme":"Other"},{"subitem_subject":"X線テレビ","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼試験","subitem_subject_scheme":"Other"},{"subitem_subject":"環境試験","subitem_subject_scheme":"Other"},{"subitem_subject":"X線計算機トモグラフィー","subitem_subject_scheme":"Other"},{"subitem_subject":"reliability criterion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solid rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"upper stage solid motor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 1 apogee motor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"scaled motor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"artificial defect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propellant notch","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propellant bubble","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"X ray TV","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"firing test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"environmental test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"X ray computed tomography","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":"上段固体ロケット・モータの信頼性評価基準に関する研究　その3:人工欠陥付き小型モータの燃焼試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"上段固体ロケット・モータの信頼性評価基準に関する研究　その3:人工欠陥付き小型モータの燃焼試験"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39804","relation_version_is_last":true,"title":["上段固体ロケット・モータの信頼性評価基準に関する研究　その3:人工欠陥付き小型モータの燃焼試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:01.990018+00:00"}