1672-9374
2009 Issue 4
Progress in combustion characteristic research of liquid rocket gelled propellants
Feng Songjiang;He Bo;Nie Wansheng
Feng Songjiang;He Bo;Nie Wansheng
..............page:1-7,13
Design and experiment of a pulse thruster with high combustion chamber pressure
Liang Shuqiang;Qin Lizi;Lin Zhen;Liu Yu;Liu Yabing;Xie Kan
Liang Shuqiang;Qin Lizi;Lin Zhen;Liu Yu;Liu Yabing;Xie Kan
..............page:8-13
Study on the LOX/methane rocket engine power cycles
Zhang Xiaoping;Li Chunhong;Ma Dongying
Zhang Xiaoping;Li Chunhong;Ma Dongying
..............page:14-20,43
..............page:21-25
Optimized design of the throttle valve core contour
Lei Heng;Cheng Yawei;Xie Ning;Zhang Chimin
Lei Heng;Cheng Yawei;Xie Ning;Zhang Chimin
..............page:26-29
Computational investigation of heat transfer for film cooling thrust chamber
Zhang Feng;Zhong Weicong
Zhang Feng;Zhong Weicong
..............page:34-37,48
Application of BP neural network in characteristics identification of frame structure
li feng ; yuan jun she
li feng ; yuan jun she
..............page:30-33
..............page:38-43
Analysis on quality stability of turbine disk die forging process
Zhang Quanming;Bai Zhoujian
Zhang Quanming;Bai Zhoujian
..............page:44-48
Formation analysis of brown red spots on the surface of sulfuric acid anodic oxide film on aluminium alloy
Zhang Yangning;Yang Zhanzheng
Zhang Yangning;Yang Zhanzheng
..............page:49-52
High and low temperature test technology of kerosene of the LOX/kerosene engine
Lai Daichu;Su Hongjun;Li Wei
Lai Daichu;Su Hongjun;Li Wei
..............page:53-58
The application of temperature measuring by infrared camera in hot firing tests for liquid rocket engine
Chi Baohua;Hong Liu;Sun Fan;Wang Mei
Chi Baohua;Hong Liu;Sun Fan;Wang Mei
..............page:59-62
..............page:封3