1006-2793
2003 Issue 2
Regulation and ground test of 100W microwave plasma thruster
yang zuo ; he hong qing ; mao gen wang ; huang xiao zuo ; han xian wei
yang zuo ; he hong qing ; mao gen wang ; huang xiao zuo ; han xian wei
..............page:75-78
Numerical study on supersonic ejector of simulated altitude test stand
xu wan wu ; tan jian guo ; wang zhen guo
xu wan wu ; tan jian guo ; wang zhen guo
..............page:71-74
A new type of hydrotest setup for filament-wound cases
wang lu xian ; du guo ru
wang lu xian ; du guo ru
..............page:68-70
Temperature test of motor combustion gas flow field with thermographic instrument
wang hong ; fu bin ; liu gui sheng ; sun mei
wang hong ; fu bin ; liu gui sheng ; sun mei
..............page:65-67
Experimental study on hydrogen peroxide and polyethylene hybrid rocket motors
du xin ; wang liang ; ge li hu ; zhang bao qing ; zhang yan
du xin ; wang liang ; ge li hu ; zhang bao qing ; zhang yan
..............page:61-64
Analysis of impact signal response spectrum of solid rocket motors
wang cui rong ; shi guang fu ; guo jun
wang cui rong ; shi guang fu ; guo jun
..............page:57-60
Erosion characterization of resin-matrix ablation materials
zuo lian sheng ; fu li kun ; liu xiao hong
zuo lian sheng ; fu li kun ; liu xiao hong
..............page:53-56
Study on A-TIG welding technology for austenitic stainless steel welding
wang wei ling ; zhang li wu ; hu shi min
wang wei ling ; zhang li wu ; hu shi min
..............page:49-52
Fitting of relaxation modulus master curve for solid propellant and W.L.F. Equation parameters
hu quan xing ; jiang yu dong ; li jian ; fu zuo zuo
hu quan xing ; jiang yu dong ; li jian ; fu zuo zuo
..............page:46-48
Numerical simulation for the axial deformation of solid propellant grains under the high acceleration shock
wei wei ; wang ning fei
wei wei ; wang ning fei
..............page:42-45
Numerical technology application in solid propellant development and production
li yi tong ; liu jian ping ; pei xiao hua
li yi tong ; liu jian ping ; pei xiao hua
..............page:38-41
Study on micro-cracking damage constitutive model of HTPB composite soltd propellant
peng wei ; zheng jian ; bai hong bai ; liu ying jie ; yang jian chun
peng wei ; zheng jian ; bai hong bai ; liu ying jie ; yang jian chun
..............page:33-37
An experimental study on the ignition and combustion characteristics of pasty propellant
zhang ming xin ; zhang sheng yong
zhang ming xin ; zhang sheng yong
..............page:30-32
Method of obtaining the burgers model parameters
meng shang yang ; tang guo jin ; lei yong jun ; zhang hai lian
meng shang yang ; tang guo jin ; lei yong jun ; zhang hai lian
..............page:27-29,45
Numerical simulation of hypersonic flow field around the reentry vehicle
zhang zhi cheng ; chen wei fang ; shi yu zhong ; wu qi fen
zhang zhi cheng ; chen wei fang ; shi yu zhong ; wu qi fen
..............page:23-26
The solid modeling technology and the grain-burning-area calculation
yan xian rong ; yu sheng chun ; wang qing guan
yan xian rong ; yu sheng chun ; wang qing guan
..............page:20-22
Effect of acceleration on the erosion of aft dome insulation of solid motors
wang shu xian ; chen lin quan ; liu ni sheng
wang shu xian ; chen lin quan ; liu ni sheng
..............page:17-19
A calculatlon analysis for structural integrity of solid propellant grains under high overload
liu zhong bing ; li feng xiang ; li yue sen ; hu chun bo
liu zhong bing ; li feng xiang ; li yue sen ; hu chun bo
..............page:12-16
Research progress of solid fuel ramjet
guo jian ; zhang wei hua ; yang tao ; xia zhi xun ; zhang zuo
guo jian ; zhang wei hua ; yang tao ; xia zhi xun ; zhang zuo
..............page:8-11,78
Effect of operation pressure on the specific impulse of tactical missile solid motors
wan shao wen ; zhao zhi min ; hu chang yu
wan shao wen ; zhao zhi min ; hu chang yu
..............page:4-7
..............page:1-3