WEKO3
アイテム
{"_buckets": {"deposit": "29c9e661-483f-4a95-a699-9ef04b636c2a"}, "_deposit": {"created_by": 1, "id": "47393", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "47393"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00047393", "sets": ["1893", "2111"]}, "author_link": ["532748", "532731", "532730", "532736", "532738", "532732", "532740", "532742", "532726", "532733", "532743", "532727", "532744", "532745", "532737", "532725", "532729", "532734", "532728", "532739", "532747", "532735", "532741", "532746"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Report of main combustion test for material of deployable nozzle"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2021-02-26", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "51", "bibliographicPageStart": "1", "bibliographicVolumeNumber": "JAXA-RR-20-005", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構研究開発報告"}, {"bibliographic_title": "JAXA Research and Development Report", "bibliographic_titleLang": "en"}]}]}, "item_3_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "本報告書は、2020年1月20日から同年2月4日にかけてJAXA宇宙科学研究所あきるの実験施設において実施した「展開ノズル材耐熱試験本試験」の試験目的から得られた実験データまでをまとめたものである。本試験ではΦ250固体モーターを使用して、開口比約50~100の部分を展開ノズルを想定したチタン合金薄板製ノズルとし、1/27及び1/31の2回の燃焼試験を実施している。試験の結果、チタン合金薄板製ノズルには若干の残留変形等は見られるものの、燃焼中の破損等には至っておらず、展開ノズルの実現に向けた貴重なデータが得られた。", "subitem_description_type": "Abstract"}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "This paper reports the purpose, plan and result of \u0027\u0027the main combustion tests for material of deployable nozzle\u0027\u0027 that was carried out from 2020/01/20 to 2020/02/04 at Akiruno Experiment Lab of ISAS/JAXA. In this test two simulated deployable nozzles made of titanium alloy sheets are used as extensions for opening ratio 50 to 100 with Φ250 solid motors and each motor was combusted on 1/27 and 1/31. As the result, the nozzles are not broken during combustion in spite of small residual plastic deformation and significant test data to develop the deployable nozzle are acquired.", "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: AA2030023000", "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-RR-20-005", "subitem_description_type": "Other"}]}, "item_3_identifier_registration": {"attribute_name": "ID登録", "attribute_value_mlt": [{"subitem_identifier_reg_text": "10.20637/00047380", "subitem_identifier_reg_type": "JaLC"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙航空研究開発機構(JAXA)"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_3_source_id_22": {"attribute_name": "ISSNONLINE", "attribute_value_mlt": [{"subitem_source_identifier": "2433-2216", "subitem_source_identifier_type": "ISSN"}]}, "item_3_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: JAXA"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 研究開発報告"}]}, "item_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: IS"}]}, "item_3_text_38": {"attribute_name": "NASA分類コード", "attribute_value_mlt": [{"subitem_text_value": "NASA分類コード: 20"}]}, "item_3_text_39": {"attribute_name": "NASA分類表目標", "attribute_value_mlt": [{"subitem_text_value": "NASA分類: Spacecraft Propulsion and Power"}]}, "item_3_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: RR"}]}, "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(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構研究開発部門第二研究ユニット(JAXA)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "nstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Research Unit II, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]}, "item_3_version_type_30": {"attribute_name": "著者版フラグ", "attribute_value_mlt": [{"subitem_version_resource": "http://purl.org/coar/version/c_970fb48d4fbd8a85", "subitem_version_type": "VoR"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "竹内, 伸介"}], "nameIdentifiers": [{"nameIdentifier": "532725", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "北川, 幸樹"}], "nameIdentifiers": [{"nameIdentifier": "532726", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "徳留, 真一郎"}], "nameIdentifiers": [{"nameIdentifier": "532727", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "戸部, 裕史"}], "nameIdentifiers": [{"nameIdentifier": "532728", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "荒川, 聡"}], "nameIdentifiers": [{"nameIdentifier": "532729", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "餅原, 義孝"}], "nameIdentifiers": [{"nameIdentifier": "532730", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "鈴木, 直洋"}], "nameIdentifiers": [{"nameIdentifier": "532731", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "芳仲, 敏成"}], "nameIdentifiers": [{"nameIdentifier": "532732", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "森下, 直樹"}], "nameIdentifiers": [{"nameIdentifier": "532733", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "岩崎, 祥大"}], "nameIdentifiers": [{"nameIdentifier": "532734", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "岩渕, 頌太"}], "nameIdentifiers": [{"nameIdentifier": "532735", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "和田, 明哲"}], "nameIdentifiers": [{"nameIdentifier": "532736", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "TAKEUCHI, Shinsuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532737", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "KITAGAWA, Koki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532738", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "TOKUDOME, Shinichiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532739", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "TOBE, Hirobumi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532740", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "ARAKAWA, Satoshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532741", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "MOCHIHARA, Yoshitaka", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532742", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "SUZUKI, Naohiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532743", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "YOSHINAKA, Toshinari", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532744", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "MORISHITA, Naoki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532745", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "IWASAKI, Akihiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532746", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "IWABUCHI, Shota", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532747", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "WADA, Asato", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "532748", "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": "2021-02-26"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "AA2030023000.pdf", "filesize": [{"value": "41.8 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 41800000.0, "url": {"label": "AA2030023000.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/47393/files/AA2030023000.pdf"}, "version_id": "2e66a702-32a9-4d39-bb7a-820de6f29c82"}]}, "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": "展開ノズル材耐熱試験本試験報告書", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "展開ノズル材耐熱試験本試験報告書"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "2111"], "permalink_uri": "https://doi.org/10.20637/00047380", "pubdate": {"attribute_name": "公開日", "attribute_value": "2021-02-26"}, "publish_date": "2021-02-26", "publish_status": "0", "recid": "47393", "relation": {}, "relation_version_is_last": true, "title": ["展開ノズル材耐熱試験本試験報告書"], "weko_shared_id": 1}
展開ノズル材耐熱試験本試験報告書
https://doi.org/10.20637/00047380
https://doi.org/10.20637/00047380c274c3d1-01d2-40bd-8052-c64b98109d82
名前 / ファイル | ライセンス | アクション |
---|---|---|
AA2030023000.pdf (41.8 MB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2021-02-26 | |||||
タイトル | ||||||
タイトル | 展開ノズル材耐熱試験本試験報告書 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
ID登録 | ||||||
ID登録 | 10.20637/00047380 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Report of main combustion test for material of deployable nozzle | |||||
著者 |
竹内, 伸介
× 竹内, 伸介× 北川, 幸樹× 徳留, 真一郎× 戸部, 裕史× 荒川, 聡× 餅原, 義孝× 鈴木, 直洋× 芳仲, 敏成× 森下, 直樹× 岩崎, 祥大× 岩渕, 頌太× 和田, 明哲× TAKEUCHI, Shinsuke× KITAGAWA, Koki× TOKUDOME, Shinichiro× TOBE, Hirobumi× ARAKAWA, Satoshi× MOCHIHARA, Yoshitaka× SUZUKI, Naohiro× YOSHINAKA, Toshinari× MORISHITA, Naoki× IWASAKI, Akihiro× IWABUCHI, Shota× WADA, Asato |
|||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門第二研究ユニット(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
nstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Research Unit II, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-20-005, p. 1-51, 発行日 2021-02-26 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本報告書は、2020年1月20日から同年2月4日にかけてJAXA宇宙科学研究所あきるの実験施設において実施した「展開ノズル材耐熱試験本試験」の試験目的から得られた実験データまでをまとめたものである。本試験ではΦ250固体モーターを使用して、開口比約50~100の部分を展開ノズルを想定したチタン合金薄板製ノズルとし、1/27及び1/31の2回の燃焼試験を実施している。試験の結果、チタン合金薄板製ノズルには若干の残留変形等は見られるものの、燃焼中の破損等には至っておらず、展開ノズルの実現に向けた貴重なデータが得られた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper reports the purpose, plan and result of ''the main combustion tests for material of deployable nozzle'' that was carried out from 2020/01/20 to 2020/02/04 at Akiruno Experiment Lab of ISAS/JAXA. In this test two simulated deployable nozzles made of titanium alloy sheets are used as extensions for opening ratio 50 to 100 with Φ250 solid motors and each motor was combusted on 1/27 and 1/31. As the result, the nozzles are not broken during combustion in spite of small residual plastic deformation and significant test data to develop the deployable nozzle are acquired. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2216 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2030023000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-20-005 |