{"created":"2023-06-20T15:13:51.774949+00:00","id":43832,"links":{},"metadata":{"_buckets":{"deposit":"aac8df31-8d09-41dd-9556-5ddc0734f7db"},"_deposit":{"created_by":1,"id":"43832","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43832"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043832","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465848"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1973-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"95","bibliographicVolumeNumber":"249","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"静止衛星打上げ能力約500kgの3段式液体ロケットについてのシステム・スタデイを行った。目的とするところはこのような液体ロケット・システムの問題点を明確にし,可能な限りそれに対する解決の方法を示すことである。風胴実験による空力特性,機体振動特性およびスロッシングの推定,推力方向制御の推定,これらに基づいた初段の安定性,誘導についての検討,計測および安全対策などについて考察を加えた。この程度の機体ではスロッシングを考慮しても初段の弾性変形の影響は飛しょうの安定性にそれ程大きくはないことが分った。また慣性誘導を採用するに際しての具体的研究開発のステップが明かになった。","subitem_description_type":"Abstract"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0249000","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 TM-249","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"宇宙研究グループ"}],"nameIdentifiers":[{"nameIdentifier":"465848","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00249.pdf","filesize":[{"value":"5.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00249.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43832/files/naltm00249.pdf"},"version_id":"83cfd993-e04d-4521-af53-5229e2884094"}]},"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":"人工衛星打上げ用ロケット・システムについての検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"人工衛星打上げ用ロケット・システムについての検討"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43832","relation_version_is_last":true,"title":["人工衛星打上げ用ロケット・システムについての検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:07:09.191840+00:00"}