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題名 | 混合火箭的發展與應用=The Development and Application of Hybrid Rocket |
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作者 | 李偉齊; | 書刊名 | 新新季刊 |
卷期 | 41:3 2013.07[民102.07] |
頁次 | 頁156-168 |
分類號 | 447.75 |
關鍵詞 | 混合火箭; 固態燃料; 氧化劑; 擴散火焰; 推進; Hybrid rocket; Solid fuel; Oxidizer; Diffusion flame; Propulsion; |
語文 | 中文(Chinese) |
中文摘要 | 合火箭推進劑主要係由固態燃料和液(氣)態氧化劑組成,亦有固態氧化劑和液(氣)燃料所組成,不過極為少見。混合火箭具有固體火箭構造簡單,又兼有液體火箭可調控推力,甚至熄火再點火的特點與能力。此外,由於混合火箭同時具備安全性高、可靠性穩、可控性好、成本低、環境衝擊少等潛在優勢,符合未來火箭推進動力系統發展方向,因此世界各國研究團隊莫不對此技術發展抱持高度的興趣,亦相繼投入本領域的研究工作。 |
英文摘要 | The hybrid rocket is mainly composed of solid fuel and liquid (gas) oxidizer, and also there is extremely few parts which are composed of solid oxidizer and liquid (gas) fuel. The structure of the hybrid rocket is as simple as the solid rocket, and just like the liquid rocket, the Hybrid rocket has a controllable thrust and the ability of re-ignition. Besides, hybrid rocket has the potential advantages of high security, stable reliability, good controllability, low cost, less environmental impact etc, which are correspond to the development of rocket propulsion system in the future. And the research teams around the world are highly interested in the technological development and studying hard in the area. |
本系統之摘要資訊系依該期刊論文摘要之資訊為主。