WEKO3
アイテム
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READ飛行実験での高々度取得スペクトルについて
https://jaxa.repo.nii.ac.jp/records/2273
https://jaxa.repo.nii.ac.jp/records/22737e41b4f3-7f5c-4665-aad9-621ca26ed2e5
名前 / ファイル | ライセンス | アクション |
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49195000.pdf (4.1 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | READ飛行実験での高々度取得スペクトルについて | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再突入 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アブレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | READ飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 淀み点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱分解 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 並進温度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動温度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷移確率 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算格子 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ablation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | READ flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stagnation point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pyrolysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | translational temperature | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibrational temperature | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transition probability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational grid | |||||
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 | Spectra observed at READ flight experiment at high altitude | |||||
著者 |
松田, 淳
× 松田, 淳× 大津, 広敬× 藤田, 和央× 鈴木, 俊之× 澤田, 恵介× 安部, 隆士× Matsuda, Atsushi× Otsu, Hirotaka× Fujita, Kazuhisa× Suzuki, Toshiyuki× Sawada, Keisuke× Abe, Takashi |
|||||
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 | ||||||
静岡大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
東北大学 | ||||||
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 | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Shizuoka University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University | ||||||
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 en : JAXA Research and Development Report 巻 JAXA-RR-05-018, 発行日 2006-03-01 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | USERSミッションでは再突入フェーズを利用して、再突入時に発生する衝撃層内の輻射光の分光スペクトル取得実験が行われた。再突入力プセルの先端ノーズ部半径は0.55mで、再突入速度は約7.5km/sであった。高度約90km付近で取得されたスペクトルからは、従来の予測では考慮されていなかったOH、NH、CHなどのアブレータと大気構成化学種との反応生成化学種からの発光が支配的であった。そこで、アブレーションを考慮したCFD解析を行い、その影響についての評価を試みた。その結果、壁面付近ではアブレータ起源化学種と大気構成化学種の反応化学種からの発光が無視できないほどの強度になることが示唆された。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | READ (Reentry Environment Advanced Diagnostics) flight experiment was conducted by making use of the reentry phase of the USERS (Unmanned Space Experiment Recovery System) mission. In this experiment, the recovery module with 0.55 m nose radius was reentered with the velocity of 7.5 km/s, and the radiation spectrum along the stagnation line was obtained. At the high altitude (about 90 km), ablator originated species such as OH, CH, NH, which were not taken into consideration in the pre-flight prediction of the spectrum, were observed mainly. In this study, the effect of the ablator originated species on the spectrum were investigated by CFD analysis. In such high altitude, it is suggested that the role of the ablator originated species can not be negligible in contrast to the preflight prediction. | |||||
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: AA0049195000 | |||||
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-05-018 |