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微小重力下での液体推薬保持技術開発のための地上模擬実験
https://jaxa.repo.nii.ac.jp/records/22445
https://jaxa.repo.nii.ac.jp/records/2244598507b78-7feb-4498-8f7f-300f9bdbcb0b
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 微小重力下での液体推薬保持技術開発のための地上模擬実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Liquid Rocket; Propellant Management; Surface Tension; Microgravity; Two-phase Flow | |||||
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 | journal article | |||||
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 | Ground Experiment for Development of Liquid Propellant Acquisition Devices under Microgravity | |||||
著者 |
杵淵, 紀世志
× 杵淵, 紀世志× 加納, 康仁× 齊藤, 靖博× 沖田, 耕一× 姫野, 武洋× Kinefuchi, Kiyoshi× Kano, Yasuhito× Saito, Yasuhiro× Okita, Koichi× Himeno, Takehiro |
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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 | ||||||
東京大学 | ||||||
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 | ||||||
The University of Tokyo | ||||||
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 |
航空宇宙技術 巻 12, p. 73-77, 発行日 2013-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | For future space transportation system development, efficient liquid propellant acquisition technologies under microgravity could berequired to realize long-term missions in orbit. Microgravity environment is generally established through drop tower, parabolic flight by airplane ororbital/suborbital experiment. These methods are large-scale or not flexible so that compact and simple method is needed for the efficientdevelopment. To respond to such request, we propose a static experiment on the ground to realize the similar static free surface under microgravity.The ground experimental result was compared with the results of two types of two-phase flow simulation codes for the verification of themethodology and discuss the characteristics of these numerical codes. We also simulated the free surface under the actual flight condition by usingthe same simulation method and result showed the validity of the experimental method. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1884-0477 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/astj.12.73 | |||||
関連名称 | info:doi/10.2322/astj.12.73 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1410086000 |