1006-2793
2001 Issue 3
..............page:57
..............page:29
Combustion Termination for S*tandard Motors Determined by Pressure Impulse Coefficient Method
bai xiao ; yuan hao ; xu xiang dong
bai xiao ; yuan hao ; xu xiang dong
..............page:75-78
The Electromagnetic Compatibi*lity Design of Electrical System for TY-3 Rocket
peng qin su ; fu chuan hui ; chen zuo bo ; wang zuo
peng qin su ; fu chuan hui ; chen zuo bo ; wang zuo
..............page:71-74
Study on the Procedure of Den*sifying C/C Composites with CLVD Process
zuo a lin ; huo xiao xu ; ma bo xin
zuo a lin ; huo xiao xu ; ma bo xin
..............page:68-70
Microstructure of Multi-m*atrix Anti-ablation C/C Composite
cui hong ; li rui zhen ; su jun ming ; li he jun ; kang mo kuang
cui hong ; li rui zhen ; su jun ming ; li he jun ; kang mo kuang
..............page:63-67
The Estabishment and Applicat*ion on Reaction Kinetic Model of Polyurethane Pr*epolymer
ren xiang zhong ; liu jian hong ; tian de yu
ren xiang zhong ; liu jian hong ; tian de yu
..............page:58-62
An Analysis on the Stress-*Strain Curves of Composite solid propellant
yang feng lin ; pang ai min ; zhang xiao ping
yang feng lin ; pang ai min ; zhang xiao ping
..............page:54-57
Experimental Studies on Effects of AP Content and Particle Size in NEPE Propellant
fang yu zhong ; li shu fen
fang yu zhong ; li shu fen
..............page:47-53
Study on GAP Based High Energy,Low Signature Propellant
li jin wei ; pang ai min ; wu jing han
li jin wei ; pang ai min ; wu jing han
..............page:42-46，53
Brief Description of a New-Concept Solid Attitude Control Motor
zhang gang chui ; ye ding you
zhang gang chui ; ye ding you
..............page:39-41
3-D Structural Analysis of SRM Grain under Operating Pressure with Filament-Wound case
tian jun liang ; zhu zu nian ; zhang shan qi ; li zuo
tian jun liang ; zhu zu nian ; zhang shan qi ; li zuo
..............page:34-38
Progress and prospect of Life Prediction Technique for Solid Rocket Motor
xing yao guo ; dong ke hai
xing yao guo ; dong ke hai
..............page:30-33，41
Models of the Fuel Surface Regression Rate in Hybrid Rocket Motor
hu jian xin ; xia zhi xun
hu jian xin ; xia zhi xun
..............page:25-29
A CAD System for Solid Propel?lant Ramjet Rocket Motor
bao fu ting ; xu dong lai ; cao jun wei
bao fu ting ; xu dong lai ; cao jun wei
..............page:19-24
Study on the Condensed Partic*al Size Distributionat SRM Nozzle Outlet
zhang hong an ; ye ding you ; hou xiao ; gao bo
zhang hong an ; ye ding you ; hou xiao ; gao bo
..............page:14-18
Design of Hybrid Filament-Wou*nd Case
chen ru xun
chen ru xun
..............page:10-13
Mode Analysis of the Nozzle i*n SRM
shi hong bin ; hou xiao ; qian qin ; zhong wei fang
shi hong bin ; hou xiao ; qian qin ; zhong wei fang
..............page:5-9
A Model of Early Warning Sate*llite Forewarning Tactical Ballistic Missile
zhao jiu fen ; wang ming hai
zhao jiu fen ; wang ming hai
..............page:1-4