1004-499X
2002 Issue 4
ASSESS ACCURACY OF ORBIT PARAMETERS ESTIMATED FROM NONLINEAR FUSION MODEL
tong li ; yi dong yun
tong li ; yi dong yun
..............page:1-5
Fisher Information Gain of Data with Applications in Test Evaluation of Missile
duan xiao jun ; wang zheng ming
duan xiao jun ; wang zheng ming
..............page:6-13
THE STUDY OF COATED PROPELLANT LOWERING GUN BALLISTIC TEMPERATURE SENSITIVITY COEFFICIENT
shi xian yang ; wang ze shan
shi xian yang ; wang ze shan
..............page:14-18
SIMPLE REACTING FLOW SIMULATION OF HYBRID ROCKET MOTOR
hu jian xin ; xia zhi xun ; zhang wei hua ; zhang zuo ; yang tao ; chen lin quan
hu jian xin ; xia zhi xun ; zhang wei hua ; zhang zuo ; yang tao ; chen lin quan
..............page:19-24,30
NUMERICAL STUDIES OF THRUST LOSS ON SERIAL BOTTOM EXHAUST-ROCKET COMPOUND EXTENDED RANGE PROJECTILES
xie zong qi ; yu ling ; wu xiao song
xie zong qi ; yu ling ; wu xiao song
..............page:25-30
NUMERICAL STUDY ON THE NON-EQUILIBRIUM FLOW OF RAM ACCELERATOR IN THE COMBUSTIVE MIXTURE GAS
liu jun
liu jun
..............page:31-35
SIMULATION AND ANALYSIS OF TWO PISTON EJECT DEVICE
wang tao ; liao zhen qiang ; jia an nian ; he da ping ; wang zuo
wang tao ; liao zhen qiang ; jia an nian ; he da ping ; wang zuo
..............page:36-39,44
THE APPLICATION OF D-S PROOF THEORY IN TARGET IDENTIFICATION
nie wei rong ; zhu ji nan ; xia hong
nie wei rong ; zhu ji nan ; xia hong
..............page:40-44
..............page:45-49
EXPERIMENTAL AND NUMERICAL SIMULATION STUDY ON JET FORM AND ITS PENETRATION INTO MULTI-LAYER METAL TARGETS
wang cheng ; huang feng lei ; zuo shou zuo
wang cheng ; huang feng lei ; zuo shou zuo
..............page:50-54
STUDY ON THE SECONDARY EXPANSION PRESSURE FIELD OF THE BURNING GAS
qian jian ping ; du xing liang ; shen tu de zhong ; sha zhi long ; li jian
qian jian ping ; du xing liang ; shen tu de zhong ; sha zhi long ; li jian
..............page:55-59,66
STUDY OF FRAGMENT PENETRATING AND DETONATE TARGET MISSILE
hong jian hua ; tao jiang yuan
hong jian hua ; tao jiang yuan
..............page:60-66
OPTIMIZE AND SIMULATION FOR DAMPING BALLISTIC COEFFICIENT OF ONE DIMENSION TRAJECTORY CORRECTION FUZE
wang bao quan ; li shi yi ; shen qiang ; guo ze rong
wang bao quan ; li shi yi ; shen qiang ; guo ze rong
..............page:67-73
ANALYSES OF SIMILARITY FOR FLIGHT TRAJECTORY OF FIN-STABILIZED PROJECTILES
wang zhong yuan ; yi wen jun ; shi jin guang
wang zhong yuan ; yi wen jun ; shi jin guang
..............page:74-77
CALCULATION OF ROTOR INDUCED FLOW UNDER THE HELICOPTER BLADES DURING THE HOVER CONDITION
wei jing biao ; sun chuan jie ; xue xiao zhong ; shu jing rong
wei jing biao ; sun chuan jie ; xue xiao zhong ; shu jing rong
..............page:78-80
EXPERIMENTAL STUDIES OF MIXED GAS IN CLOSED COMBUSTION BOMB
zou rui rong ; yuan ya xiong ; weng chun sheng
zou rui rong ; yuan ya xiong ; weng chun sheng
..............page:81-83
STUDY ON THE LASER SYSTEM FOR REAL-TIME MEASURING THE MUZZLE VELOCITY OF PROJECTILE
chen xin ; cao cong yong ; liu ying shun
chen xin ; cao cong yong ; liu ying shun
..............page:84-86,96
A NEW VIEWPOINT ON TEST METHOD OF PROVING GROUND
tian gui jun ; yuan ya xiong
tian gui jun ; yuan ya xiong
..............page:87-91
STUDY ON THE TECHNIQUE OF AMMUNITION SYSTEM OF WEAPON WITH EXTRA-HIGH FIRING RATE PROJECTILE SCREEN
yu bin
yu bin
..............page:92-96