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ATREXエンジンへのC/C複合材料の適用
https://jaxa.repo.nii.ac.jp/records/33351
https://jaxa.repo.nii.ac.jp/records/33351ab54be4c-53d1-41ca-ad08-5baf14b72544
名前 / ファイル | ライセンス | アクション |
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SA0200124.pdf (1.3 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ATREXエンジンへのC/C複合材料の適用 | |||||
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_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Applications of Carbon-Carbon Composites to an ATREX Engine for a Future TSTO Space Vehicle | |||||
著者 |
八田, 博志
× 八田, 博志× 後藤, 健× 向後, 保雄× 福田, 博× 佐藤, 哲也× 棚次, 亘弘× Hatta, Hiroshi× Goto, Ken× Kougo, Yasuo× Fukuda, Hiroshi× Sato, Tetsuya× Tanatsugu, Nobuhiro |
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著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
東京理科大学 | ||||||
著者所属 | ||||||
東京理科大学 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo University of Science | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo University of Science | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science (ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science | |||||
書誌情報 |
宇宙科学研究所報告. 特集: ATREXエンジンの研究開発 巻 46, p. 205-224, 発行日 2003-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Feasibility studies were carried out aiming at the application of carbon/carbon (C/C) composites to a turbine disk, heat exchangers, and a plug nozzle for an ATREX engine intended for use in a future TSTO space vehicle. In these applications, the maximum temperature was estimated to be about 1500C. In order to withstand this high temperature, attempts were made to utilize three-dimensionally reinforced C/C composites. The most serious problem encountered in the application of C/Cs to the turbine disk was the loss of fragments of the composite located near the outer periphery due to strong centrifugal force, which resulted in severe vibration due to rotational imbalance. The heat exchangers and plug nozzle have complex shapes in order to realize a large heat exchanging area. Joined structures were explored for these components. The principal effort in these applications has been placed on finding structures requiring low joining strength and developing materials with low gas leakage. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0285-9920 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00354485 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0200124000 |