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[1]谭永华.中国重型运载火箭动力系统研究[J].火箭推进,2011,37(01):1-6.
　TAN Yong-hua.Research on power system of heavy launch vehicle in China[J].Journal of Rocket Propulsion,2011,37(01):1-6.
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中国重型运载火箭动力系统研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 37 期数: 2011年01期 页码: 1-6 栏目: 专论与综述 出版日期: 2011-02-15
Title:
Research on power system of heavy launch vehicle in China
文章编号:
1672-9374(2011)01-0001-06
作者:
谭永华
航天推进技术研究院，陕西 西安 710100
Author(s):
TAN Yong-hua
Academy of Aerospace Propulsion Technology, Xi’an 710100, China
关键词:
载人登月; 深空探测; 重型运载火箭; 液体火箭发动机; 液氧煤油发动机; 液氧液氢发动机
分类号:
V43-34
文献标志码:
A
摘要:
分析了未来航天发展趋势，指出为实现载人登月和深空探测，发展重型运载火箭，研制大推力火箭发动机势在必行。提出了中国重型运载火箭主动力——600吨级液氧煤油发动机和200吨级液氧液氢发动机的总体方案，确定了发动机的主要参数，明确了发动机的关键技术，考虑了发动机的研制条件，进行了发动机研制策划。根据中国的技术水平和经济实力，有望在2020年前后完成两种发动机研制。
Abstract:
The development trend of future aerospace industry is analyzed. The necessity of developing the heavy launch vehicles and high thrust rocket engines to realize the manned moonfall and deep space exploration is described. The main power system of heavy launch vehicles of China is planned. A integrated scheme of 600 t LOX/kerosene rocket engine and 200 t LOX/LH2 rocket engine is put forward. The primary parameters of the two engines are chosen. The key technology and development condition of the rocket engines is analyzed. The development effort is schemed. The development of the two engines will be completed in about 2020 according to the level of technology and industrial base.

参考文献/References:

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备注/Memo

收稿日期：2010-12-03；修回日期：2010-01-06
基金项目：中国航天科技集团公司支撑项目
作者简介： 谭永华（1964—），男，研究员，研究领域为液体动力系统总体设

更新日期/Last Update: 1900-01-01