Home >>2015 03 issue list
GAO Zhao-hui1, 2, LIU Yu1, XIAO Xiao2, WANG Xiao-wei2, SHEN Lin2
Challenge to propulsion technology for vertical landing reusable launch vehicle
Abstract(1186)
PDF: 351KB(764)
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TIAN Li-cheng, WANG Xiao-yong, ZHANG Tian-ping
Application and development trend of space electric propulsion technology
Abstract(774)
PDF: 527KB(1045)
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SHEN Zhi-shuai1, 2, RUAN Hai-jun1, 2
Pneumopump technology and its application in space propulsion system
Abstract(997)
PDF: 1692KB(666)
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HUANG Qi-yin, WANG Xing-guo, LIU Shang, LI Miao-ting
Simulation and test study on starting box of LOX/kerosene rocket engine
Abstract(906)
PDF: 2122KB(534)
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ZHOU Yi-peng, ZHU Ding-qiang
Numerical calculation of radiative heat flux on nozzle wall of liquid propellant rocket engine
Abstract(781)
PDF: 2180KB(497)
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NAN Xiang-Jun1, ZHANG Rui2, ZHANG Liu-huan1
Effect of wall surface heat dissipation on performance of supersonic nozzle
Abstract(722)
PDF: 2138KB(518)
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SHI Duan, HU Xiao-ping, YU Meng, WANG Zheng-kai
Application of case-based reasoning method in design of thrust chamber of liquid rocket engine
Abstract(709)
PDF: 341KB(590)
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ZHANG Xiao-guang1, CHENG Cheng2, LIU Yu3
Cold flow test of outflow influence on vehicle with aerospike nozzle
Abstract(769)
PDF: 2111KB(419)
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LIU Hai-li1, ZHANG Li-qiang1, LI Xue-hua1, Lü Zhi-quan2
Influence of volute case type for low-specific-speed pump on pump performance
Abstract(764)
PDF: 2636KB(524)
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PAN Zhao-yi, CAI Gang, MA Shuang-min, SONG Guo-xin
Research on thermal protection behavior of silicide coating on Nb-W alloys used at high temperature
Abstract(1250)
PDF: 2214KB(662)
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MA Ying, WANG Liang
Design research of U-E-type metal sealing
Abstract(605)
PDF: 289KB(519)
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LI Tong, LIU Zhan-guo, DOU Yu, JIN Ai-ping
Field calibration technology for torque of turbo pump hydraulic test system
Abstract(827)
PDF: 1767KB(622)
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MA Jun-qiang, YANG Si-feng, DAI Fang-li
RVM-based fault prediction method for liquid rocket engine test stand
Abstract(811)
PDF: 796KB(737)
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YUAN Jie, PAN Liang
Reliability assessment of a certain insensitive igniter based on startup time-sequence of rocket engine
Abstract(837)
PDF: 772KB(496)
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SHEN Chuan-bing, SU Hang, ZHU Zi-yong
Control system for liquid rocket engine heat-vacuum test based on PLC and WinCC
Abstract(953)
PDF: 252KB(540)
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LIU Wan-long, SUN Shu-jiang, SHAO Shuai, TIAN Guo-hua, ZHU Hao-wei
Application of vibrator in thrust vector measurement turntable for orbit-control engine of satellite
Abstract(838)
PDF: 1148KB(593)
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CHEN Wen-li, MA Jun-qiang, YANG Si-feng, TIAN Guo-hua
Prediction on thrust calibration slope based on FIG-SVR for attitude control rocket engine
Abstract(736)
PDF: 705KB(547)
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LIU Xiao-jie, DU Yong-qing, ZHANG He-ping, LU Yan
Design of measurement and control system for burner test bench based on LabVIEW and PLC
Abstract(802)
PDF: 1183KB(648)
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