The Reliable and Intelligent Propulsion Pressurization System of the Long March 7 Launch Vehicle

被引:1
作者
FAN Ruixiang [1 ]
DENG Xinyu [2 ]
SHAO Yetao [2 ]
YANG Haoliang [2 ]
TIAN Yurong [2 ]
机构
[1] China Academy of Launch Vehicle Technology
[2] Beijing Institute of Astronautical Systems Engineering
关键词
high reliability; intelligent; pressurization; propulsion system;
D O I
暂无
中图分类号
V475.1 [运载火箭];
学科分类号
082503 ;
摘要
The reliable and intelligent propulsion pressurization system is one of the key technologies of new Chinese generation launch vehicles; a high reliability design is an important guarantee for the success of launching. This paper analyzes the domestic and overseas liquid launch vehicles in the area of propulsion pressurization systems, based on comprehensive analysis, demonstrating the reliable and intelligent propulsion pressurization system of the Long March 7(Simplified as LM-7) has been raised. By applying a full chain redundancy design, setting proper pressure control bandwidth and control mode reconstruction under extreme fault conditions, the reliability and adaptability of the propulsion pressurization system has enhanced significantly. In addition, the complete system has been verified by the first two flights of LM-7.
引用
收藏
页码:13 / 18
页数:6
相关论文
共 5 条
[1]  
Gaseous- helium requirements for the discharge of liquid hydrogen from a 3 96-meter- (13-fx") diameter spherical tank. STOCHL J R,MALOY J E,MASTERS A P,et al. NASA TN D-7019 . 1970
[2]  
The pressurization system of liquid rocket. LIAO S Y. . 2007
[3]  
Pressurization systems for liquid rockets. NASA SPACE VEHICLE DESIGN CRITERIA. NASA SP 8112 .
[4]  
Liquid helium storage for Ariane 5main stage oxygen tank pressurization. Teissier A,Liquide A. AIAA 95-2956 .
[5]  
Liquid helium storage for Ariane 5main stage oxygen tank pressurization. Teissier A,Liquide A. AIAA 95-2956 .