| 大型液体火箭发动机的最新发展 |
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| 引用本文： | 毛根旺. 大型液体火箭发动机的最新发展[J]. 推进技术, 1995, 16(1): 1-6 |
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| 作者姓名： | 毛根旺 |
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| 作者单位： | 西北工业大学航天工程学院 |
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| 摘 要： | 根据美国对ＳＳＭＥ和ＳＴＭＥ的改进设计以及前苏联、欧洲和日本分别对ＲＤ－０１２０、Ｖｕｌｃａｉｎ和ＬＥ－７发动机的开发研究，探讨在研制未来大推力液体火箭发动机（ＬＲＭ）中各国的指导思想和设计原则，分析世界在这一领域的发展动向。
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| 关 键 词： | 重型运载火箭，氢氧发动机，高压补燃火箭发动机，航天飞机主发动机，助推火箭发动机，发展趋势分析 |
THE LATEST DEVELOPMENTS OF LARGESCALE LIQUID ROCKET MOTORS |
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| Mao Genwang. THE LATEST DEVELOPMENTS OF LARGESCALE LIQUID ROCKET MOTORS[J]. Journal of Propulsion Technology, 1995, 16(1): 1-6 |
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| Authors: | Mao Genwang |
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| Abstract: | n recent years, the space shuttle main engine (SSME) and the spacetransportation main engine (STME) have been improved in the U. S. A., in addition, the RD-170, Vulcain and LE-7 LRM have respectively been developed by theformer Soviet Union, Europe and Japan. According to these improvements and developments, this paper would inquire into the guide thinkings and design principlesof the various countries in the developments of the future large-scale LRM, andthen analyse the world's new development trend in this field. |
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| Keywords: | Heavy lift launch vehicle Hydrogen oxygen enging High pressers staged combustion rocket engine Space shuttle main engine Booster rocket enging Trend analysis |
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