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高速軌道を用いた着陸実験システムの構築
https://jaxa.repo.nii.ac.jp/records/49474
https://jaxa.repo.nii.ac.jp/records/4947413254e92-7ce6-4a27-b1fe-52c8ab4470dc
名前 / ファイル | ライセンス | アクション |
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SA6000184018.pdf (1.1 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2023-05-23 | |||||
タイトル | ||||||
タイトル | 高速軌道を用いた着陸実験システムの構築 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Rocket Sled | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reusable Rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Landing | |||||
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 | Development of Landing Experiment System using Rocket Sled | |||||
著者 |
江口, 光
× 江口, 光× 岡野, 裕× 柴田, 拓馬× 中田, 大将× EGUCHI, Hikaru× OKANO, Hiro× SHIBATA, Takuma× NAKATA, Daisuke |
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著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS) | |||||
書誌情報 |
令和4年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium FY2022 発行日 2023-01 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 令和4年度宇宙輸送シンポジウム(2023年1月12日-13日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)) , 相模原市, 神奈川県 | |||||
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 | Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The flight demonstration of reusable rockets requires landing technologies such as deceleration and descent by engine throttling and shock absorption by landing legs. To achieve these landing technologies, this study aims to create a landing and descent environment using a rocket sled for reusable rockets. In this paper, we describe the landing and descent environment that can be achieved with the proposed experimental system, and also describe its current development status. | |||||
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: SA6000184018 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | STCP-2022-018 |