パルスデトネーションエンジンの新観測ロケットへの応用
| Autor: | FUKIBA, Katsuyoshi, KAWASAKI, Akira, MAEDA, Shinichi |
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| Jazyk: | japonština |
| Rok vydání: | 2023 |
| Zdroj: | 令和4年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2022. |
| Popis: | 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 Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan This study proposes to use air-breathing pulse detonation engines in the new sounding rocket of JAXA. Air-breathing pulse detonation engines with high specific impulse have great possibilities to improve the rocket performance. However, the engines have never operated as independent propulsion systems. Two new ideas are introduced in this study to use detonation engines in practice. 資料番号: SA6000184016 STCP-2022-016 |
| Databáze: | OpenAIRE |
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