WEKO3
アイテム
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アーク加熱風洞によるREVアブレータの研究開発
https://jaxa.repo.nii.ac.jp/records/2321
https://jaxa.repo.nii.ac.jp/records/232155837f66-d09b-433c-a537-f2dddcd23cf0
名前 / ファイル | ライセンス | アクション |
---|---|---|
48710005.pdf (2.4 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | アーク加熱風洞によるREVアブレータの研究開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アーク加熱風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力加熱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アブレータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 回収機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リエントリモジュール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | USERSカプセル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | USERSミッション | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | arc wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic heating | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ablator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | recovery vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry module | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | USERS capsule | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | USERS mission | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Research and development of REV ablator in arc windtunnel | |||||
著者 |
奥山, 圭一
× 奥山, 圭一× 加藤, 純郎× 山田, 哲哉× Okuyama, Keiichi× Kato, Sumio× Yamada, Tetsuya |
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著者所属 | ||||||
川崎重工業 航空宇宙カンパニー | ||||||
著者所属 | ||||||
川崎重工業 航空宇宙カンパニー | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. Aerospace Company | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. Aerospace Company | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
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: USERS REVカプセルの開発研究および飛行後解析 en : JAXA Research and Development Report: Research and Development of USERS REV Capsule and its Post-flight Analysis 巻 JAXA-RR-04-045, p. 55-75, 発行日 2005-03-31 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | REV was the first reentry capsule developed through pure domestic technology and successfully recovered. REV is thermally protected against the severe aerodynamic heating by carbon-phenolic ablator material. The present paper describes the feature of the heating test in the arc wind tunnel and the ablator characteristics clarified during the research and development process of the REV heat shield. Because the heat flux anticipated on the stagnation surface is about 2 MW/sq m, the dominant surface recession mechanism is identified to be in the reaction control region. The thermochemical reaction data have been acquired through three arc-heater facilities with different enthalpy level for calibration and tuning of the ablation analysis code. The thermomechanical behavior of the ablator under the high heat flux environment such as delamination, or spallation also has been investigated for functional safety of the heat shield. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0048710005 | |||||
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-04-045 |