1004-499X
2002 Issue 1
FUSION OF TRAJECTORY TRACKED BY RELAY OPTICAL MEASURE SYSTEM
he ming ke ; wang zheng ming
he ming ke ; wang zheng ming
..............page:1-7,26
THE CLOSED VESSEL COMBUSTION AND BALLISTIC PROPERTY STUDY OF LOW TEMPERATURE SENSITIVITY HIGH ENERGY NITROAMINE
shi xian yang ; he wei dong ; wang ze shan
shi xian yang ; he wei dong ; wang ze shan
..............page:8-13
THE 2-D NUMERICAL SIMULATION ON PENETRATIONS OF AN OVALHEADED PROJECTILE INTO CONCRETE TARGETS
li yong chi ; yuan fu ping ; hu xiu zhang ; zhu lin fa ; wang dao rong
li yong chi ; yuan fu ping ; hu xiu zhang ; zhu lin fa ; wang dao rong
..............page:14-19
INVESTIGATION ON RESIDUAL VELOCITIES OF LAMINATED COMPOSITE TARGETS SUBJECTED TO BALLISTIC IMPACT
xiong jie ; gu bo hong ; wang shan yuan
xiong jie ; gu bo hong ; wang shan yuan
..............page:20-26
STUDY AND 3D SIMULATION OF KE-ROD DIRECTIONAL DISPENSE
lu yong gang ; jiang jian wei ; jiang dao jian
lu yong gang ; jiang jian wei ; jiang dao jian
..............page:27-31
NUMERICAL SIMULATION OF PRE-TWISTED TUNGSTEN PROJECTILE PENETRATING STEEL TARGET
xu rui huai ; hu xiu zhang ; hu shi sheng
xu rui huai ; hu xiu zhang ; hu shi sheng
..............page:32-36
APPLICATION CRITERION OF OSCILLATOR FOR FUZE AND STUDY OF IT'S PERFORMANCE ON EXPERIMENTS
sun quan yi ; jiang xiao hua ; zhang he
sun quan yi ; jiang xiao hua ; zhang he
..............page:37-40,48
GRID GENERATION AND SIMULATION OF APFSDS AND SABOTS
tan jun jie ; zhang jun ; wu pin
tan jun jie ; zhang jun ; wu pin
..............page:41-44
STUDY ON AERODYNAMICS OF BODIES WITH PLANE NOSE IN SUPERSONIC FLOWS
liu jun ; huang lin
liu jun ; huang lin
..............page:45-48
APPLICATION OF AMMUNITION ENGINEER SIMULATION BASED ON VRML TECHNOLOGY
li chao jun ; lu yong gang ; sui shu yuan
li chao jun ; lu yong gang ; sui shu yuan
..............page:49-53
THEORETICAL CALCULATION OF STRENGTH OF MULTI-LAYERED CYLINDER
zhang yue ; fan xin min ; kong de ren
zhang yue ; fan xin min ; kong de ren
..............page:54-57
THE PROGRAMMABLE PULSED POWER SUPPLY SYSTEM AND ITS APPLICATIONIN ON THE ELECTROTHERMAL LIGHT GAS LAUNCHER
meng shao liang ; li bao ming
meng shao liang ; li bao ming
..............page:58-62
EXPERIMENTAL INVESTIGATION ON THERMAL FEATURES OF ARMORED VEHICLES
han yu ge ; li qiang ; xuan yi min
han yu ge ; li qiang ; xuan yi min
..............page:63-68
EFFECTIVE EVALUATION OF MULTIPLE LAUNCHER ROCKET WEAPON SYSTEM
ma yan qin ; ma da wei ; yu peng xiao
ma yan qin ; ma da wei ; yu peng xiao
..............page:69-72
OPTIMIZATION OF PNEUMATIC DEVICE SYSTEM
dai long cheng ; xuan yi min ; yin jian
dai long cheng ; xuan yi min ; yin jian
..............page:73-76,83
..............page:77-83
TO DETERMINE DIFFERENT POINTS OF BALLISTIC MEASUREMENT FOR TRAJECTORY CORRECTION
wang zhong yuan ; tu si hua ; ai dong min ; yi wen jun ; wang liang ming
wang zhong yuan ; tu si hua ; ai dong min ; yi wen jun ; wang liang ming
..............page:84-87
INFLUENCE OF AMBIENT PRESSURE ON BASE BLEED
ding ze sheng ; chen shao song ; liu ya fei ; cao ding gui
ding ze sheng ; chen shao song ; liu ya fei ; cao ding gui
..............page:88-92
THE APPLICATION OF DIMENSION ANALYSIS ON MAKING ABSOLUTE CALIBRATION MODEL OF TRANSDUCERS
kong de ren ; zhu ming wu ; li yong xin ; liu de qiu
kong de ren ; zhu ming wu ; li yong xin ; liu de qiu
..............page:93-96