1672-9374
2009 Issue 3
..............page:61-64
The anti-interference technology of thermocouple channel used in rocket engine test system
Liu Chao;Feng Bin;Wang Lixin;Zhang Jinmin
Liu Chao;Feng Bin;Wang Lixin;Zhang Jinmin
..............page:55-60
Propellant inlet temperature control for cryogenic rocket engine tests
Cao Wenqing;Tan Hailin;Li Wei
Cao Wenqing;Tan Hailin;Li Wei
..............page:52-54,60
Rotational speed measurement of liquid rocket engine pumps
Feng Xikai;Li Hui;Li Wei
Feng Xikai;Li Hui;Li Wei
..............page:47-51
Study on closed loop control of rocket engine inlet pressure based on expert control system
Zhu Danbo;Nan Weilin;Xue Huijian
Zhu Danbo;Nan Weilin;Xue Huijian
..............page:42-46
Technology of relayed test with different oxidizers for liquid rocket engine
Zhao Jianjun;Liu Hongwei
Zhao Jianjun;Liu Hongwei
..............page:38-41
The method and application of small gaseous mass flow rate measurement system
Cao Zhicheng;Fei Lisen
Cao Zhicheng;Fei Lisen
..............page:34-37
Simulation of the pressurizing process of propellant feed system
Jin Xiaowei;Sun Liang;Ma Jian;Li Ping
Jin Xiaowei;Sun Liang;Ma Jian;Li Ping
..............page:30-33,46
..............page:26-29
Numerical investigation of spray in high speed airflow
Ma Tianju;Luan Xiting;Hong Liu
Ma Tianju;Luan Xiting;Hong Liu
..............page:21-25
..............page:15-20
Investigation on local
overheating of the film cooling ring for LOX/kerosene high pressure chamber
Lü Fazheng
Lü Fazheng
..............page:11-14
Structure pattern analysis of gas-gas injector
Du Zhenggang;Gao Yushan;Cai Guobiao
Du Zhenggang;Gao Yushan;Cai Guobiao
..............page:6-10
Geometry design and analysis of the high-speed rotational plate inducer
Chen Hui;Zhang Enzhao;Tan Yonghua;Li Bin
Chen Hui;Zhang Enzhao;Tan Yonghua;Li Bin
..............page:1-5