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(1428)
PDF: 351KB(1097)
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TIAN Li-cheng, WANG Xiao-yong, ZHANG Tian-ping
Application and development trend of space electric propulsion technology
Abstract(1055)
PDF: 527KB(1222)
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SHEN Zhi-shuai1, 2, RUAN Hai-jun1, 2
Pneumopump technology and its application in space propulsion system
Abstract(1176)
PDF: 1692KB(727)
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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(1218)
PDF: 2122KB(589)
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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(895)
PDF: 2180KB(558)
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NAN Xiang-Jun1, ZHANG Rui2, ZHANG Liu-huan1
Effect of wall surface heat dissipation on performance of supersonic nozzle
Abstract(837)
PDF: 2138KB(581)
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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(835)
PDF: 341KB(653)
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ZHANG Xiao-guang1, CHENG Cheng2, LIU Yu3
Cold flow test of outflow influence on vehicle with aerospike nozzle
Abstract(1058)
PDF: 2111KB(481)
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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(885)
PDF: 2636KB(584)
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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(1444)
PDF: 2214KB(870)
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MA Ying, WANG Liang
Design research of U-E-type metal sealing
Abstract(668)
PDF: 289KB(576)
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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(943)
PDF: 1767KB(704)
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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(926)
PDF: 796KB(806)
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YUAN Jie, PAN Liang
Reliability assessment of a certain insensitive igniter based on startup time-sequence of rocket engine
Abstract(960)
PDF: 772KB(552)
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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(1112)
PDF: 252KB(610)
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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(950)
PDF: 1148KB(643)
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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(841)
PDF: 705KB(610)
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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(910)
PDF: 1183KB(724)
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