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レーザーアブレーションによる飛翔体推進の効率化
https://jaxa.repo.nii.ac.jp/records/38078
https://jaxa.repo.nii.ac.jp/records/38078f3ae9420-6a8d-40fe-90b7-f55b68b40027
名前 / ファイル | ライセンス | アクション |
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nalsp0053041.pdf (2.5 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | レーザーアブレーションによる飛翔体推進の効率化 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レーザアブレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 発射体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 標的 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 運動量結合係数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | YAGレーザ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値計算 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laser ablation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | projectile | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | target | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | momentum coupling coefficient | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerospace vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | YAG laser | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical calculation | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | The study on the efficiency of projectile propulsion driven by laser ablation | |||||
著者 |
青木, 圭一
× 青木, 圭一× 矢部, 孝× 中川, 順達× 尾形, 陽一× Aoki, Keiichi× Yabe, Takashi× Nakagawa, Masamichi× Ogata, Yoichi |
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著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
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特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001 巻 53, p. 245-250, 発行日 2002-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, the numerical calculations of laser propulsion for space vehicle are discussed. For calculating the behavior of ablation, it is necessary to do with the solid, the liquid and the gas at the same time. This process was calculated with the hydrocode based on a highly-accurate scheme CIP-CUP (Cubic-Interpolated Pseudoparticle Combined Unified Procedure) method. With this scheme, the efficiency by C(sub m) (the momentum coupling coefficient) is evaluated for the cases of single pulse and some target shapes. In order to confirm the result, experiments were performed with a pendulum and a semi-conductor load-cell. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0032819042 | |||||
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 SP-53 |