1006-2793
2002 Issue 1
An analytical determination method of the burning time for solid rocket motors
lu jiang he ; di jiang yuan
lu jiang he ; di jiang yuan
..............page:76-78
Research of instantaneous thrust recovery technology of solid rocket motors
wang cui rong ; shi guang fu ; di jiang yuan
wang cui rong ; shi guang fu ; di jiang yuan
..............page:73-75
An experimental investigation on rocket ejector at low speed
liu pei jin ; he guo qiang ; chen jian ; huang sheng hong ; wang guo hui
liu pei jin ; he guo qiang ; chen jian ; huang sheng hong ; wang guo hui
..............page:69-72
Study on the UV curing of epoxy acrylate resin modified with polysiloxane
he min ; zhang zuo ; wang xiao jie
he min ; zhang zuo ; wang xiao jie
..............page:65-68
Effect of resin content on properties of aramid fiber/e poxy composites
wang bin ; jin zhi hao ; qiu zhe ming ; liu ai hua
wang bin ; jin zhi hao ; qiu zhe ming ; liu ai hua
..............page:61-64
..............page:58-60
Elastoplastic problem of interfacial crack on bi material
xiao wan shen ; tang guo jin ; zhou jian ping
xiao wan shen ; tang guo jin ; zhou jian ping
..............page:55-57
Propellant burning rate calculation with improved predictions
mu han mo de ma zha er yi ke ba er ; wang liang
mu han mo de ma zha er yi ke ba er ; wang liang
..............page:51-54
..............page:46-50
Action mechanisms of special functional agents in composite solid propellants-(I) HTPB/AP system
tang han xiang ; liu xiu lan ; wu zuo
tang han xiang ; liu xiu lan ; wu zuo
..............page:41-45
Study on combustion properties of HTPB propellant containing nitramine under high and low pressure
jia xiao feng ; su chang yin ; lv gong lian
jia xiao feng ; su chang yin ; lv gong lian
..............page:38-40
..............page:33-37,50
Study on prilled ammonium dinitramide(ADN)
ma yue ; zhang hai lin
ma yue ; zhang hai lin
..............page:29-32
Effect of potassium salt flame suppressors on the ther mal decomposition behavior of the combustion catal ysts used in solid propellant
zhao feng qi ; chen pei ; li shang wen ; yin cui mei ; liu zi ru
zhao feng qi ; chen pei ; li shang wen ; yin cui mei ; liu zi ru
..............page:26-28,32
A control method of the ignition Pressure peak
wang li ; tang han yun
wang li ; tang han yun
..............page:24-25
A study on the application of high combustion velocity motors in boost phase penetration technology of strate-gic missiles
jie hong yu ; zhang wei hua ; li xiao bin ; yang tao
jie hong yu ; zhang wei hua ; li xiao bin ; yang tao
..............page:20-23
Optimization of parameters in the shock wave system of the regular reflection for supersonic flow
tao gang
tao gang
..............page:16-19
A finite-element analysis of microscopic stress distri bution and microdamage growth in composite solid propel lant
peng wei ; zhou jian ping ; zhao wei chang ; meng shang yang
peng wei ; zhou jian ping ; zhao wei chang ; meng shang yang
..............page:12-15
Effects of nozzle contour in convergent section and throat on mass flow rate
chen lin quan ; li yan fang ; hou xiao ; dong xin gang
chen lin quan ; li yan fang ; hou xiao ; dong xin gang
..............page:10-11,19
Numerical simulation on flow field of double-nozzle solid rocket motors
liu jun ; guo jian
liu jun ; guo jian
..............page:8-9,15
One-dimensional interior ballistic calculation of solid rocket motors with dual burning rate propellant
bao fu ting ; zhao fei ; li jin xian
bao fu ting ; zhao fei ; li jin xian
..............page:5-7
The technologies of reliability assessment of solid rocket motors
liu peng ; zhang ping
liu peng ; zhang ping
..............page:1-4