1000-1328
2001 Issue 4
MISSILE CLOBBER PROBABILITY'S RELATION WITH SELECTION OF MAIN PARAMETERS
zhou zuo ; guo qi feng ; zhou hui zhong
zhou zuo ; guo qi feng ; zhou hui zhong
..............page:100-104
..............page:95-99
THE STRUCTURAL ELIMINATION METHOD IN FAULT DIAGNOSIS BASED ON MATHEMATICS MODEL AND MEASURE PARAMETER
li jia wen ; zhang chun liang ; zhang zhen peng ;kolomentsev a.i
li jia wen ; zhang chun liang ; zhang zhen peng ;kolomentsev a.i
..............page:90-94
FAULT DETECTION FOR POWER SYSTEM USED IN SPACE AEROCRAFT
zhang chun liang ; zhang zhen peng ; yuan jun zuo ; zhang ben bin
zhang chun liang ; zhang zhen peng ; yuan jun zuo ; zhang ben bin
..............page:85-89
INVESTIGATION ON GAS DYNAMIC RESONANCE IGNITION TECHNOLOGY FOR LIQUID PROPELLANT ROCKET ENGINE
zhang guo zhou ; tong xiao yan ; liang guo zhu ; ma bin ; cheng xian chen
zhang guo zhou ; tong xiao yan ; liang guo zhu ; ma bin ; cheng xian chen
..............page:81-84
AN RAPID APPROACH FOR FLIGHT VEHICLE CONFIGURATION SCHEME SELECTION
wang shu he ; he zuo shu ; ren yan rong ; li xiang qian
wang shu he ; he zuo shu ; ren yan rong ; li xiang qian
..............page:76-80
STATIC DEFORMATION CONTROL OF PLATELIKE ADAPTIVE STRUCTURES CONSIDERING SMOOTHNESS REQUIREMENT
huang hai ; sun wen jun
huang hai ; sun wen jun
..............page:71-75
ANADAPTIVEDAMPING-VARIABLEVIBRATIONDAMPER WITH MAGNETORHELOGICAL SUSPENSIONS
sun bing ; nie jing xu
sun bing ; nie jing xu
..............page:67-70
INVESTIGATION ON THE IGNITION METHODS OF AEROSPIKE NOZZLE ENGINE
tong xiao yan ; ma bin ; zhang guo zhou
tong xiao yan ; ma bin ; zhang guo zhou
..............page:62-66
WORK PROCESS AND PERFORMANCE EXPERIMENT OF A LOW POWER NITROGEN ARCJET
tang hai bin ; zhang zheng ke ; liu yu ; dai wu ye
tang hai bin ; zhang zheng ke ; liu yu ; dai wu ye
..............page:56-61
AN ERROR COMPENSATION METHOD FOR SOLAR PANEL SUBSTRATE PLANENESS MEASURING SYSTEM
fang jian cheng ; zhao jian hui ; yu wen bo ; shen gong xun
fang jian cheng ; zhao jian hui ; yu wen bo ; shen gong xun
..............page:50-55
BUCKLING OF COMPOSITE SANDWICH PLATES
peng wei bin ; zhu sen yuan ; hu ze bao ; liu ying qing
peng wei bin ; zhu sen yuan ; hu ze bao ; liu ying qing
..............page:41-49
VECTRIX AND ITS APPLICATION IN MODELING OF TARGET STATE ESTIMATION PROBLEM
chen wan chun ; xiao ye lun ; yang jian min
chen wan chun ; xiao ye lun ; yang jian min
..............page:34-40
EXPERIMENTAL AND NUMERICAL STUDIES ON A UNIT OF AEROSPIKE NOZZLE
liu yu ; dai wu ye ; tang hai bin ; cheng xian chen ; ma bin ; wang yi bai ; zuo li zi
liu yu ; dai wu ye ; tang hai bin ; cheng xian chen ; ma bin ; wang yi bai ; zuo li zi
..............page:27-33
THE EFFECT OF FLOW FIELD CHANGING ON LINEAR PLUG NOZZLE
dai wu ye ; liu yu ; zhang zheng ke ; zuo li zi ; wang yi bai
dai wu ye ; liu yu ; zhang zheng ke ; zuo li zi ; wang yi bai
..............page:20-26
NUMERICAL SIMULATION OF VACUUM PLUME WITH CHEMICAL REACTION
cai guo zuo ; guo jing jing ; zhuang feng gan ; zhu xiao lan
cai guo zuo ; guo jing jing ; zhuang feng gan ; zhu xiao lan
..............page:13-19
ORBITAL DYNAMICAL CHARACTERISTICS AND CONFIGURATION DESIGN OF FORMATION FLYING SATELLITES
xiao ye lun ; zhang xiao min
xiao ye lun ; zhang xiao min
..............page:7-12
..............page:1-6