Journal of Solid Rocket Technology 2004 Issue 1 Virtual instrument technology based on hybrid programming of VC++ and MATLAB

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Journal of Solid Rocket Technology
1006-2793
2004 Issue 1

Virtual instrument technology based on hybrid programming of VC++ and MATLAB
zhang zhen hai ; fang shu zhou ; han zhen hai

..............page:84-86

Test and research of nozzle closure made of hard foamed plastics
tu xiao chang ; wang zhan li ; wang xiao juan

..............page:81-83

Determination of the physical properties of functional gradient materials
zhang yan ; liu ni sheng ; chen lin quan ; wang shu xian ; liu yong qiong

..............page:77-80,83

Effect of short fiber filler on the properties of NBR-matrix insulator
song chong jian ; zhang zuo ; mo ji an

..............page:73-76

The erosive property of copper-infiltrated graphite throat insert
su jun ming ; chen lin quan ; wang shu xian ; hou xiao ; li gui lin

..............page:69-72

Preparation and properties of EPDM/montmorillonite nanocomposites
li wei ; huang yu dong ;ahmadi s j

..............page:64-68

Study on longitudinal tensile properties of F-12/CF hybrid composites
zeng jin fang ; qiao sheng ru ; qiu zhe ming ; ma zheng ; wang ting wu

..............page:60-63

Study on the erosion mechanism of copper-infiltrated graphite throat insert
chen lin quan ; wang shu xian ; zhang sheng yong ; hou xiao

..............page:57-59

Study on mechanical properties of PEO binder propellants
si zuo ming

..............page:53-56,86

Effect of AP particle size and coating on combustion of boron
wang ying hong ; li zuo zuo ; hu song qi ; xiao xiu you

..............page:50-52,68

Stability analysis of the interfacial debonded crack between propellant and liner of solid rocket motor grains
meng shang yang ; tang guo jin ; lei yong jun

..............page:46-49,72

Development of formulation and process for high density and high strength HTPB propellant
li zuo she ; su chang yin ; li zuo zuo ; zhang ai ke

..............page:41-45

Microscale hotspot model of solid propellant under mechanical impact
chen guang nan

..............page:37-40

Advances in high energy density matter of furazan series
zhang de xiong ; zhang yan ; wang zuo

..............page:32-36

Study on secondary combustion chamber air-inlet scheme of unchoked solid rocket ramjet
hu jian xin ; xia zhi xun ; wang zhi ji ; guo jian ; zhang zuo ; luo zhen bing ; zuo wan bo

..............page:28-31

Research on low frequency unstable combustion of H2O2-PE hybrid rocket motors
du xin ; wang liang

..............page:24-27

Study on the low-pressure self-destruction effect of an analog solid rocket motor
liu ping ; yin ya xia

..............page:22-23,36

Internal ballistic calculation of solid rocket motors
he jing xuan ; yu zhen yong ; sun li qing ; hou xiao ; zhao jin ping

..............page:20-21,45

Optimization design of performance and cost for high-pressure solid rocket motors
li xiao bin ; jie hong yu ; qing long ; zhang wei hua ; chen ya qin ; sun bing

..............page:16-19

The thermal condition analysis of stage separation for a multistage solid rocket before the nozzle exit cone extend
han li xia ; tian wei ping ; le fa ren ; yu zhen yong

..............page:12-15

Effects of the nozzle divergent cone contour on solid rocket motor performance
chen lin quan ; li yan fang ; wang jian ru ; hou xiao

..............page:9-11

Numerical investigation on diffusion afterburning of RBCC in ejector mode
wang guo hui ; he guo qiang ; liu pei jin ; cai ti min

..............page:5-8

Design and trial of a rocket erection device
cheng yang min ; yan li min ; wang xiao jun

..............page:1-4