1672-9374
2007 Issue 4
..............page:封3
Research on liquid oxygen density measurement
Zhao Wanming
Zhao Wanming
..............page:56-62
..............page:52-55
Temperature measuring technologies of rocket combustor by an infrared camera
Hong Liu;Zhong Weicong;Wang Mei
Hong Liu;Zhong Weicong;Wang Mei
..............page:47-51
Investigation on corrosion behavior and mechanism of carbon tetrachloride to 1J116 alloy
Zhang Wanxin;Chi Chun;Zhang Yong
Zhang Wanxin;Chi Chun;Zhang Yong
..............page:41-46
Development status of stationary plasma thruster and its key technologies
Liu Wenyi;Bai Wenping;Wang Hongxuan
Liu Wenyi;Bai Wenping;Wang Hongxuan
..............page:36-40
Finite element analysis of the overturning process of titanium diaphragm for propellant tank
Zhu Zhihua;Hu Xiaoping;Chen Xianglin
Zhu Zhihua;Hu Xiaoping;Chen Xianglin
..............page:32-35,51
..............page:28-31
Simulation of the second combustor internal flowfield for a solid-propellant ducted rocket
Xu Yingjun;Gao Feng;Wang Peng
Xu Yingjun;Gao Feng;Wang Peng
..............page:23-27,46
Research of xenon ion thrusters beam current distribution characteristic
Chen Linying;Song Renwang
Chen Linying;Song Renwang
..............page:20-22
The optimal design of solid rocket motors
Wang Peng;Li Xuchang;Xu Yingjun
Wang Peng;Li Xuchang;Xu Yingjun
..............page:16-19
Experimental investigation of the apparent viscosity and the shear rate of gelled propellant in straight round pipe
Zuo Bo;Zhang Mengzheng
Zuo Bo;Zhang Mengzheng
..............page:12-15
Effects of the isolator on the exit parameters of two-dimension inlet
Huang Wei;Luo Shibin;Wang Zhenguo
Huang Wei;Luo Shibin;Wang Zhenguo
..............page:8-11,15
Hot-firing tests on aerospike nozzles
Wang Changhui;Liu Yu
Wang Changhui;Liu Yu
..............page:1-7