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2011
06 issue list
HANG Guan-rong, KANG Xiao-lu
Propulsion system of USA AEHF military communication satellite and its application on AEHF-1 satellite
Abstract
(
717
)
PDF: 541KB
(
714
)
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JIANG Wen-long, YANG Cheng-hu, LIN Qing-guo
Development of high performance 490 N apogee engine for satellites
Abstract
(
899
)
PDF: 343KB
(
713
)
+ Favorites
LI Wen-long, LI Ping, GUO Hai-bo
Research progresses on turbulent mixing and combustion for air-turbo-rocket engine
Abstract
(
1048
)
PDF: 464KB
(
678
)
+ Favorites
CHENG Yu-feng, NIE Wan-sheng, FENG Song-jiang
Effects of turbulent and spray models on combustion process simultion of LOX/GH2 rocket engine
Abstract
(
952
)
PDF: 364KB
(
521
)
+ Favorites
CHEN Zhan, HE Wei-tao, WANG Ke-li
Elimination of low-frequency unstable combustion phenomenon of a certain engine
Abstract
(
888
)
PDF: 209KB
(
523
)
+ Favorites
CHEN Wen-qu, LI Lu-lu, CHEN Jian
Development of pneumatic pressure regulator with metal diaphragm
Abstract
(
921
)
PDF: 289KB
(
735
)
+ Favorites
ZHANG Feng, ZHONG Wei-cong, ZHANG Wei-jing
Effect of wall thickness on throat wall temperature of space small thrust engines
Abstract
(
711
)
PDF: 217KB
(
549
)
+ Favorites
SONG Ya-fei
1
, GAO Feng
1
, YANG Xiao-qiu
2
Dynamic simulation for effect of incoming flow Mach number on internal flow field of fluidic thrust vectoring nozzle
Abstract
(
1084
)
PDF: 290KB
(
624
)
+ Favorites
HU Song-qi, WANG Peng-fei, LIU Kai, YOU Chen-xun, GUAN Peng
Pilot study on solid fuel containing paraffin
Abstract
(
769
)
PDF: 239KB
(
455
)
+ Favorites
LI Bo, LIU He
Technological research on machining of brazed centrifugal impeller
Abstract
(
795
)
PDF: 258KB
(
547
)
+ Favorites
ZHU Zi-yong, SUN Wan-min, WANG Zhan-lin
Numerical simulation of gas replacement process in LH2 tank of test-bed
Abstract
(
659
)
PDF: 473KB
(
453
)
+ Favorites
LI Zhi-xun
Design of performance testing system for gas relief valve of an attitude control engine
Abstract
(
895
)
PDF: 364KB
(
586
)
+ Favorites
LI Zheng-bing, WANG Xiao-li, JIANG Xing-jia
Automatic calibration technology of pressure sensor in rocket engine
Abstract
(
800
)
PDF: 180KB
(
506
)
+ Favorites
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