中国航天主动力液体火箭发动机技术进展(英文)
发布时间:2021-05-24 09:42
Liquid propellant rocket engines for a launch vehicle are an essential aerospace technology, representing the advanced level of hi-tech in a country. In recent years, China’s aerospace industry has made remarkable achievements, and liquid rocket engine technology has also been effectively developed. In this article, the development processes of China’s liquid rocket engines are discussed. Then, the performance features of China’s new generation liquid rocket engines as well as the flight tests o...
【文章来源】:Aerospace China. 2020,21(02)
【文章页数】:8 页
【文章目录】:
1 INTRODUCTION
2 STATUS OF CHINA’S IN-SERVICE LIQUID MAIN POWER UNITS
2.1 Main Power Units of LM-2,LM-3 and LM-4
2.2 Main Power Units of the New-Generation Launch Vehicles LM-5,LM-6,and LM-7
2.2.1 Introduction to LM-5,LM-6,and LM-7
2.2.2 Features of the new generation main powers
3 RECENT PROGRESS OF CHINA’S LIQUID MAIN POWER UNIT
3.1 YF-100 Modifier Engine
3.2 4800 kN LOX/kerosene Rocket Engine
3.3 2000 kN LOX/LH2 Rocket Engine
3.4 LOX/methane Rocket Engines
4 CONCLUSIONS
【参考文献】:
期刊论文
[1]我国大推力补燃氢氧发动机研究进展[J]. 孙纪国,岳文龙. 上海航天. 2019(06)
[2]我国大推力氢氧发动机发展思考[J]. 郑孟伟,岳文龙,孙纪国,郑大勇. 宇航总体技术. 2019(02)
[3]Development of China’s New Generation Launch Vehicles[J]. QIN Tong,XU Lijie,LI Pingqi,LIU Jiajia. 空间科学学报. 2018(05)
[4]液氧甲烷发动机重复使用关键技术发展研究[J]. 郑大勇,颜勇,孙纪国. 导弹与航天运载技术. 2018(02)
[5]关于重型运载火箭若干问题的思考[J]. 龙乐豪,郑立伟. 宇航总体技术. 2017(01)
[6]Innovation and Outlook of the New Generation of Cryogenic and Quick-Launch Launch Vehicle[J]. ZHANG Weidong,LIU Chang,WANG Wei. Aerospace China. 2017(02)
[7]重型运载火箭总体技术研究[J]. 张智,容易,秦曈,孙冀伟. 载人航天. 2017(01)
[8]新一代运载火箭50吨级氢氧发动机研制进展[J]. 郑大勇,王维彬,乔桂玉. 导弹与航天运载技术. 2016(05)
[9]大推力氢氧发动机关键技术及解决途径[J]. 郑大勇,陶瑞峰,张玺,向猛. 火箭推进. 2014(02)
[10]大推力液体火箭发动机研究[J]. 谭永华. 宇航学报. 2013(10)
本文编号:3203987
【文章来源】:Aerospace China. 2020,21(02)
【文章页数】:8 页
【文章目录】:
1 INTRODUCTION
2 STATUS OF CHINA’S IN-SERVICE LIQUID MAIN POWER UNITS
2.1 Main Power Units of LM-2,LM-3 and LM-4
2.2 Main Power Units of the New-Generation Launch Vehicles LM-5,LM-6,and LM-7
2.2.1 Introduction to LM-5,LM-6,and LM-7
2.2.2 Features of the new generation main powers
3 RECENT PROGRESS OF CHINA’S LIQUID MAIN POWER UNIT
3.1 YF-100 Modifier Engine
3.2 4800 kN LOX/kerosene Rocket Engine
3.3 2000 kN LOX/LH2 Rocket Engine
3.4 LOX/methane Rocket Engines
4 CONCLUSIONS
【参考文献】:
期刊论文
[1]我国大推力补燃氢氧发动机研究进展[J]. 孙纪国,岳文龙. 上海航天. 2019(06)
[2]我国大推力氢氧发动机发展思考[J]. 郑孟伟,岳文龙,孙纪国,郑大勇. 宇航总体技术. 2019(02)
[3]Development of China’s New Generation Launch Vehicles[J]. QIN Tong,XU Lijie,LI Pingqi,LIU Jiajia. 空间科学学报. 2018(05)
[4]液氧甲烷发动机重复使用关键技术发展研究[J]. 郑大勇,颜勇,孙纪国. 导弹与航天运载技术. 2018(02)
[5]关于重型运载火箭若干问题的思考[J]. 龙乐豪,郑立伟. 宇航总体技术. 2017(01)
[6]Innovation and Outlook of the New Generation of Cryogenic and Quick-Launch Launch Vehicle[J]. ZHANG Weidong,LIU Chang,WANG Wei. Aerospace China. 2017(02)
[7]重型运载火箭总体技术研究[J]. 张智,容易,秦曈,孙冀伟. 载人航天. 2017(01)
[8]新一代运载火箭50吨级氢氧发动机研制进展[J]. 郑大勇,王维彬,乔桂玉. 导弹与航天运载技术. 2016(05)
[9]大推力氢氧发动机关键技术及解决途径[J]. 郑大勇,陶瑞峰,张玺,向猛. 火箭推进. 2014(02)
[10]大推力液体火箭发动机研究[J]. 谭永华. 宇航学报. 2013(10)
本文编号:3203987
本文链接:https://www.wllwen.com/kejilunwen/dongligc/3203987.html