1672-9374
2015 Issue 3
Challenge to propulsion technology for vertical landing reusable launch vehicle
GAO Zhao-hui;,LIU Yu;,XIAO Xiao;,WANG Xiao-wei;,SHEN Lin;
GAO Zhao-hui;,LIU Yu;,XIAO Xiao;,WANG Xiao-wei;,SHEN Lin;
..............page:1-6,45
Application and development trend of space electric propulsion technology
TIAN Li-cheng;,WANG Xiao-yong;,ZHANG Tian-ping;
TIAN Li-cheng;,WANG Xiao-yong;,ZHANG Tian-ping;
..............page:7-14
Pneumopump technology and its application in space propulsion system
SHEN Zhi-shuai;,RUAN Hai-jun;
SHEN Zhi-shuai;,RUAN Hai-jun;
..............page:15-20
Simulation and test study on starting box of LOX/kerosene rocket engine
HUANG Qi-yin;,WANG Xing-guo;,LIU Shang;,LI Miao-ting;
HUANG Qi-yin;,WANG Xing-guo;,LIU Shang;,LI Miao-ting;
..............page:21-26
Numerical calculation of radiative heat flux on nozzle wall of liquid propellant rocket engine
ZHOU Yi-peng;,ZHU Ding-qiang;
ZHOU Yi-peng;,ZHU Ding-qiang;
..............page:27-32,51
Effect of wall surface heat dissipation on performance of supersonic nozzle
NAN Xiang-Jun;,ZHANG Rui;,ZHANG Liu-huan;
NAN Xiang-Jun;,ZHANG Rui;,ZHANG Liu-huan;
..............page:33-38
Application of case-based reasoning method in design of thrust chamber of liquid rocket engine
SHI Duan;,HU Xiao-ping;,YU Meng;,WANG Zheng-kai;
SHI Duan;,HU Xiao-ping;,YU Meng;,WANG Zheng-kai;
..............page:39-45
Cold flow test of outflow influence on vehicle with aerospike nozzle
ZHANG Xiao-guang;,CHENG Cheng;,LIU Yu;
ZHANG Xiao-guang;,CHENG Cheng;,LIU Yu;
..............page:46-51
Influence of volute case type for low-specific-speed pump on pump performance
LIU Hai-li;,ZHANG Li-qiang;,LI Xue-hua;,Lü Zhi-quan;
LIU Hai-li;,ZHANG Li-qiang;,LI Xue-hua;,Lü Zhi-quan;
..............page:52-58
Research on thermal protection behavior of silicide coating on Nb-W alloys used at high temperature
PAN Zhao-yi;,CAI Gang;,MA Shuang-min;,SONG Guo-xin;
PAN Zhao-yi;,CAI Gang;,MA Shuang-min;,SONG Guo-xin;
..............page:59-65
Design research of U-E-type metal sealing
MA Ying;,WANG Liang;
MA Ying;,WANG Liang;
..............page:66-72
Field calibration technology for torque of turbo pump hydraulic test system
LI Tong;,LIU Zhan-guo;,DOU Yu;,JIN Ai-ping;
LI Tong;,LIU Zhan-guo;,DOU Yu;,JIN Ai-ping;
..............page:73-79,86
RVM-based fault prediction method for liquid rocket engine test stand
MA Jun-qiang;,YANG Si-feng;,DAI Fang-li;
MA Jun-qiang;,YANG Si-feng;,DAI Fang-li;
..............page:80-86
Reliability assessment of a certain insensitive igniter based on startup time-sequence of rocket engine
YUAN Jie;,PAN Liang;
YUAN Jie;,PAN Liang;
..............page:87-92,97
Control system for liquid rocket engine heat-vacuum test based on PLC and WinCC
SHEN Chuan-bing;,SU Hang;,ZHU Zi-yong;
SHEN Chuan-bing;,SU Hang;,ZHU Zi-yong;
..............page:93-97
Application of vibrator in thrust vector measurement turntable for orbit-control engine of satellite
LIU Wan-long;,SUN Shu-jiang;,SHAO Shuai;,TIAN Guo-hua;,ZHU Hao-wei;
LIU Wan-long;,SUN Shu-jiang;,SHAO Shuai;,TIAN Guo-hua;,ZHU Hao-wei;
..............page:98-102
..............page:封3
Prediction on thrust calibration slope based on FIG-SVR for attitude control rocket engine
CHEN Wen-li;,MA Jun-qiang;,YANG Si-feng;,TIAN Guo-hua;
CHEN Wen-li;,MA Jun-qiang;,YANG Si-feng;,TIAN Guo-hua;
..............page:103-107
Design of measurement and control system for burner test bench based on LabVIEW and PLC
LIU Xiao-jie;,DU Yong-qing;,ZHANG He-ping;,LU Yan;
LIU Xiao-jie;,DU Yong-qing;,ZHANG He-ping;,LU Yan;
..............page:108-112