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Aerospace Shanghai
1006-1630
2006 Issue 4
Air Bubble Judgement of Liquid Floated Flexible Pendulum Accelerometer
DU Wei;CHEN Min-hua;JI Ming-hua
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page:61-64
Forming Technology Improvement of Winding Extendible Nozzle Exit for Some Tactical Missile Engine
WANG Jian-hua
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page:58-60
The Efficiency Evaluation of Air Defense Weapon System Based on Queuing Theory
ZHANG Sheng-tao;LOU Shou-chun;WANG Jun
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page:55-57,64
The Simulation Analysis on Variable Structure Control of Some Antiaircraft Missile
LI Wei-zhong;ZHANG Ji-hua;ZHANG Chun-ming;LIU Jian-feng
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page:49-54
A Numerical Simulation of Aerodynamic Drag of Solar Array Spreading on Ground
CHEN Chang-gan;GAO Hong
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page:44-48
Application Research of FSW Welding Process for Joining Propellant Tanks in New Generation Launch Vehicle
XING Mei-yuan;YAO Jun-shan;LIU Jie
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page:39-43
Application of MEMS-Based Microchannel Cooling System in Micro/Nano Satellite Thermal Control
SHAO Bao-dong;SUN Zhao-wei
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page:34-38
Analysis of Supersonic Thermo-Flutter of the Wing with High Angle of Attack
SHI Xiao-ming;YANG Bing-yuan
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page:30-33
Advanced Control Method Research for Lift Reentry Flight
LI Ke-feng;TIAN yuan;REN Zhang
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page:27-29,33
Scattering Coefficient Calculation of Dielectric Ocean Rough Surface with Different Wind Speed
YAN Pei-wen;TONG Chuang-ming;DENG Fa-sheng
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page:23-26
Application of Accelerometer Data to Orbit Determination
HAN Jian;YANG Long;DONG Xu-rong
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page:20-22,26
Research on the Negative Damp Zero Network of Launch Vehicle's Attitude Control System
LIN Jie
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page:13-19
Research on Autonomous Navigation for Satellite during New-Moon Period Based on SEMOI
ZHANG Yan;JING Wu-xing
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page:8-12
Key Techniques of TT&C for On-Orbit TDRS (Part 1)
LI Yu-heng;LIU Ning-ning
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page:1-7