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。
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.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1995年第1期1-6,共6页
Journal of Propulsion Technology
关键词
运载火箭
氢氧发动机
助推火箭
液体推进剂
Heavy lift launch vehicle, Hydrogen oxygen enging, High pressers staged combustion rocket engine, Space shuttle main engine, Booster rocket enging, Trend analysis
