Technical Innovation of LH2/LOX Rocket Engines in China

Chengzhi Li, Bingtao Ma
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引用次数: 2

Abstract

: This paper provides a detailed introduction to and analysis of the course of China’s technological innovation in liquid hydrogen/liquid oxygen (LH2/LOX) rocket engines from a historical point of view. It starts with the investigation of LH2/LOX rocket engines by relevant departments of the Chinese Academy of Sciences in the 1960s and their preliminary achievements. Then, the policy decision concerning LH2/LOX engine development, the project approval of the Long March-3 (Chang Zheng-3, CZ-3) rocket, and the process of developing LH2/LOX engines are analyzed in detail, followed by an introduction to and summary of the development situation and technical innovation characteristics of China’s LH2/LOX engines as they grew from 4 tons to 8 tons, and finally to 50 tons. Finally, the paper briefly analyzes the innovation experience connected with China’s LH2/LOX engines.
中国LH2/LOX火箭发动机技术创新
本文从历史的角度详细介绍和分析了中国液氢/液氧(LH2/LOX)火箭发动机技术创新的历程。从20世纪60年代中国科学院有关部门对LH2/LOX火箭发动机的研究及其初步成果说起。然后,详细分析了我国LH2/LOX发动机研制的政策决策、长征三号(长征三号,长征三号)火箭的立项以及LH2/LOX发动机的研制过程,介绍和总结了我国从4吨发展到8吨的LH2/LO克斯发动机的发展情况和技术创新特点,最后达到50吨。最后,简要分析了我国LH2/LOX发动机的创新经验。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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0.50
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95
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