WEKO3
アイテム
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高圧液酸ターボポンプ試験設備タービン駆動系
https://jaxa.repo.nii.ac.jp/records/44214
https://jaxa.repo.nii.ac.jp/records/44214dbbd0a5b-3790-4011-ae3a-1fd4be5faf1e
名前 / ファイル | ライセンス | アクション |
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naltm00631.pdf (1.9 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 | 高圧液酸ターボポンプ試験設備タービン駆動系 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Test Facility; Rocket Turbine; Turbopump; LE-7; H-II | |||||
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 | Turbine Drive System of the High Pressure LOX Turbopump Test Facility | |||||
著者 |
渡辺, 義明
× 渡辺, 義明× 長谷川, 敏× 上條, 謙二郎× 橋本, 亮平× 坂本, 雄二郎× 戸根, 重幸× WATANABE, Yoshiaki× HASEGAWA, Satoshi× KAMIJO, Kenjiro× HASHIMOTO, Ryohei× SAKAMOTO, Yuujiro× TONE, Shigeyuki |
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著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
株式会社神戸製鋼所 | ||||||
著者所属 | ||||||
三菱重工業株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe Steel, LTD. | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries, LTD. | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所資料 en : Technical Memorandum of National Aerospace Laboratory 巻 631, p. 17, 発行日 1991-01 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | わが国においては現在大型ロケットH-IIの開発が進んでいる。このロケットには同じく開発中の大型液酸・液水エンジンLE-7が使用される。LE-7エンジンには高圧・大流量の液体酸素を燃焼器に供給する液酸ターボポンプが必要になる。航空宇宙技術研究所は同ターボポンプの研究開発を担当している。1985年角田支所に高圧液酸ターボポンプ試験設備を整備した。本報告は,同設備のタービン駆動系について記述したものであり,特に高圧水素ガス/液体酸素ガス発生器の作動シーケンスや高圧・大流量のタービン排ガス処理装置について詳しく記述した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A large launch vehicle, called the H-II, has been developed in Japan, and will use the LE-7 liquid oxygen/liquid hydrogen engine which is also under development. The engine requires a liquid oxygen (LOX) turbopump which supplies the main combustion chamber with a large quantity of high pressure liquid oxygen. The National Aerospace Laboratory (NAL) has been in charge of the research and development of this turbopump, with a test facility having been constructed at the Kakuda Research Center in 1985. The facility's turbine drive system is discussed, with emphasis on the control sequence of the high presssure gaseous hydrogen/liquid oxygen gas generator, and also on the turbine exhaust gas disposal equipment which designed to handle high pressures and large flows. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTM0631000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TM-631 |