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Aerospace Shanghai
1006-1630
2000 Issue 5
bai qi qing he
..............page:55
METHOD OF MAIN ENGINE POWER GENERATION OF MISSILE LAUNCHING VEHICLE WITH OUTSIDE POWER SUPPLY
CHEN Yong-yan;GAO Shang-fei;ZHANG Zhen-hua
..............page:59-61
THE WASTE TREATMENT OF ROCKET PROPELLANT
ZHENG Hong-jian;MA Yan;CHEN Chuan-xin
..............page:56-58
EXPERIMENTAL RESEARCH ON J INTEGRAL CRITERION OF PROPELLANT/LINER BOND
ZHAO Guang-hui;QIANG Hong-fu;ZHANG Yong-jing
..............page:23-27
SOLUTIONS OF CONSTRAINED MODE AND UNCONSTRAINED MODE OF FLEXIBLE STRUCTURE
SHAN Jin-jun;GUAN Ying-zi;WANG Feng-ming;LIU Dun
..............page:19-22,27
STUDY ON CONTAMINATION CAUSED BY PLUME FLOW FROM THE TRANSFER ORBITAL ROCKET OF SATELLITE
CHENG Xiao-li;MAO Ming-fang;YAN Xi-qin
..............page:15-18
TERMINAL GUIDANCE USING SYNTHETIC DISCRIMINANT CORRELATION RECOGNITION
LI Xiao-jian;SUN Hong-hui;HE Jun-fa
..............page:10-14
THE BUILDING METHOD OF SYSTEM ERROR MODEL
QIN Rong-hua
..............page:5-9
SPACEBORNE SAR IMAGING WITH SPECAN ALGORITHM
ZHENG Ming-jie
..............page:1-4
THE RF ENVIRONMENT EMULATION FOR FREQUENCY HOPPING RADAR AND ITS CRITICAL TECHNOLOGY
LI Shang-sheng;JIANG Yong-hua
..............page:47-50
PERFORMANCE OF 35Ah NICKEL-HYDROGEN BATTERY FOR AEROSPACE
WU Yong-xian;LIU Tong-chang;LU Rong;ZHU Kai
..............page:37-41