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高エネルギーX線CTを用いた再使用ロケットエンジン燃焼室の非破壊検査
https://jaxa.repo.nii.ac.jp/records/38771
https://jaxa.repo.nii.ac.jp/records/38771b17421c8-dc73-430d-b645-89b9abe4227b
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-08-15 | |||||
タイトル | ||||||
タイトル | 高エネルギーX線CTを用いた再使用ロケットエンジン燃焼室の非破壊検査 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Nondestructive Inspection | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Combustion Chamber | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | X-ray CT | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Image Analysis | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Nondestructive Inspection of Reusable Rocket Engine Combustor using High-energy X-ray Computed Tomography | |||||
著者 |
佐藤, 正喜
× 佐藤, 正喜× 橋本, 知之× 森谷, 信一× 木村, 俊哉× 八木下, 剛× 高木, 寛之× 藤井, 拓也× 佐藤, 克利× Sato, Masaki× Hashimoto, Tomoyuki× Moriya, Shin-ichi× Kimura, Toshiya× Yagishita, Tsuyoshi× Takagi, Hiroyuki× Fujii, Takuya× Sato, Katsutoshi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
株式会社日立製作所 | ||||||
著者所属 | ||||||
株式会社日立製作所 | ||||||
著者所属 | ||||||
株式会社日立製作所 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi, Ltd | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
第59回宇宙科学技術連合講演会講演集 en : Proceedings of 59th Space Sciences and Technology Conference 発行日 2015-10-07 |
|||||
関係URI | ||||||
識別子タイプ | URI | |||||
関連識別子 | https://www.jsass.jp/conference/sstc59.php | |||||
関連名称 | https://www.jsass.jp/conference/sstc59.php | |||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第59回宇宙科学技術連合講演会(2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The regenerative cooling combustion chamber of a liquid propellant rocket engine is one of the critical components to limit the life of engine. Especially for the reusable rocket engine combustor, it is important to develop an effective nondestructive inspection technique to assure its life. JAXA/ISAS developed a reusable LOX/LH2 rocket engine for the Reusable Sounding Rocket and conducted 142 times of engine firings. In the series of firing tests, 4 times of nondestructive inspection of the combustion chamber was carried out using a high-energy X-ray CT system of Hitachi, Ltd. By making full use of image analysis technique, the deformation of chamber inner wall and the distribution of chamber wall thickness can be evaluated, and their transitional progress due to the repeated engine firing tests are also clarified. | |||||
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 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11800503 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1600029000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2015-4443 |