| 我国大推力氢氧发动机发展思考 |
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| 作者姓名： | 郑孟伟 岳文龙 孙纪国 郑大勇 |
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| 作者单位： | 北京航天动力研究所 |
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| 摘 要： | 对国内外氢氧发动机发展历程进行综述,指出了国外氢氧发动机的发展规律和国内氢氧发动机的发展现状和差距。结合我国重型运载火箭应用需求、国内氢氧发动机技术基础和航天强国发展目标,论证了我国大推力氢氧发动机选择补燃循环技术方案是恰当选择,还进一步给出了我国220t级补燃循环氢氧发动机的技术参数,提出了未来发展展望。
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| 关 键 词： | 大推力氢氧发动机 补燃循环 技术方案 发展展望 |
Discussion on Chinese Large-Thrust Hydrogen/Oxygen Rocket Engine Development |
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| Authors: | ZHENG Mengwei YUE Wenlong SUN Jiguo and ZHENG Dayong |
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| Institution: | Beijing Aerospace Propulsion Institute,Beijing Aerospace Propulsion Institute,Beijing Aerospace Propulsion Institute and Beijing Aerospace Propulsion Institute |
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| Abstract: | In this paper, the worldwide development history of Hydrogen/Oxygen rocket engine is reviewed. The development rules are summarized, The status and gap of domestic Hydrogen/Oxygen rocket engine is pointed out. Combined with the application demand of Chinese heavy lunch vehicle, the present technical status, and the development goal for powerful nation in space, the large-thrust staged combustion cycle Hydrogen/Oxygen engine is the appropriate choice. In addition, the technical parameters of a 220-ton staged combustion cycle Hydrogen/Oxygen engine are given out. The future development prospects are put forward. |
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| Keywords: | Large-thrust Hydrogen/Oxygen rocket engine Staged combustion cycle Design |
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