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損傷力学に基づく人工衛星用二液式スラスタ燃焼器のクリープ疲労解析
https://jaxa.repo.nii.ac.jp/records/22699
https://jaxa.repo.nii.ac.jp/records/226992c47dddc-917e-468f-979c-7fc38a1fd9e3
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-06-24 | |||||
タイトル | ||||||
タイトル | 損傷力学に基づく人工衛星用二液式スラスタ燃焼器のクリープ疲労解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Damage mechanics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Bipropellant thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Niobium alloy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | High temperature | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Creep | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Fatigue | |||||
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 | Damage mechanics based creep fatigue analysis of combustion chamber for satellite's bipropellant thruster | |||||
著者 |
升岡, 正
× 升岡, 正× 都井, 裕× 池田, 博英× Masuoka, Tadashi× Toi, Yutaka× Ikeda, Hirohide |
|||||
著者所属 | ||||||
東京大学大学院工学系研究科 | ||||||
著者所属 | ||||||
東京大学生産技術研究所 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
School of Engineering, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Industrial Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 日本機械学会 | |||||
出版者(英) | ||||||
出版者 | The Japan Society of Mechanical Engineers | |||||
書誌情報 |
日本機械学会論文集 en : Transactions of the JSME (in Japanese) 巻 82, 号 835, p. 15-00667, 発行日 2016-03-15 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Creep - fatigue analyses based on the concept of continuum damage mechanics were conducted for the combustion chamber used in a satellite’s bipropellant thruster. The previously identified models and material parameters for the niobium alloy (C103) which is used as the combustion chamber’s material were extended to deal with the prediction of the creep - fatigue behavior and the chamber life of a bipropellant thruster. The thrust force of 22 N thruster was selected for FEM analyses and post damage calculations. The analyses in different injection modes of continuation and pulse were conducted to evaluate their influence on the chamber’s life. The maximum temperatures on a chamber surface were also changed for two patterns of 1250 C and 1500 C. The combustion chamber life was evaluated for the different surface temperature. The analysis results show that the calculated chamber’s life of continuous injection at 1500 C was shorter than that at 1250 C because of plasticity damage. The analysis results also show that the major damage mode was creep and fatigue damage was very little in pulse injection. From the results, it is expected that the used models and determined material parameters can predict the mechanical features and creep - fatigue life for the combustion chamber of a bipropellant thruster. | |||||
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 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2187-9761 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1299/transjsme.15-00667 | |||||
関連名称 | info:doi/10.1299/transjsme.15-00667 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1610089000 |