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Advanced Stability Analysis of Propulsion System for Future Launch Vehicles
https://jaxa.repo.nii.ac.jp/records/38624
https://jaxa.repo.nii.ac.jp/records/38624e7a2389a-8350-4543-a848-d453b1e6efe7
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
AC1400043000 (468.2 kB)
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| Item type | 会議発表論文 / Conference Paper(1) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | Advanced Stability Analysis of Propulsion System for Future Launch Vehicles | |||||||||
| 言語 | en | |||||||||
| 言語 | ||||||||||
| 言語 | eng | |||||||||
| キーワード | ||||||||||
| 言語 | en | |||||||||
| 主題Scheme | Other | |||||||||
| 主題 | Liquid Propellant; Propulsion; Stability; POGO; Cavitation Surge | |||||||||
| 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 | |||||||||
| 著者 |
堀, 秀輔
× 堀, 秀輔
× Hori, Shusuke
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| 著者所属 | ||||||||||
| 宇宙航空研究開発機構(JAXA) | ||||||||||
| 著者所属（英） | ||||||||||
| en | ||||||||||
| Japan Aerospace Exploration Agency(JAXA) | ||||||||||
| 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 |
en : Asian Joint Conference on Propulsion and Power 2010 発行日 2010-03 |
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| 会議概要（会議名, 開催地, 会期, 主催者等）（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | Asian Joint Conference on Propulsion and Power 2010（March 4-6, 2010. Miyazaki Kanko Hotel), Miyazaki-City, Miyazaki, JapanAbstract: A time-domain response analysis model has been developed to evaluate the stability of rocket propulsion systems with a cavitating inducer. Also a simple cost-effective experimental method to estimate the transfer functions of cavitating pump, which are key factors in determining the propulsion system response, is proposed. The presented dynamic model and the transfer function estimation method are verified by comparing the results with the data acquired in development tests of the real rocket engine. It is shown that these will be powerful tools for a quick, cost-effective and reliable development of a stable propulsion system in the future. | |||||||||
| 権利 | ||||||||||
| 権利情報 | (C)2010 一般社団法人日本航空宇宙学会 | |||||||||
| 著者版フラグ | ||||||||||
| 出版タイプ | AM | |||||||||
| 出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||||||
| 資料番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | 資料番号: AC1400043000 | |||||||||
