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《Chinese Journal of Explosives & Propellants》 2009-03
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Study on Software of Solid Propellant Burning Rate Prediction Based on one-dimensional Steady-state Reaction Gas Flow

FENG Feng,CHEN Jun,ZHENG Ya, SONG Hong-chang(School of Mechanical Engineering,Nanjing University of Science and Technology,Nanjing 210094,China)  
Based on the model of one-dimensional steady-state reaction gas flow,the correction factors of burning rate related to double base propellant,modified double base propellant and composite solid propellant were summed up,the application scope of theoretical combustion model was broadened.Using Visual C++and Microsoft Access for the development tools,the software of solid propellant burning rate prediction(SPRS) was completed by the structural parameters of chemical bonds.The software was based on system of Windows XP,user-friendly,easy to use,and with the functions of data updating and information querying.The burning rates and pressure indexs could been calculated when the chemical compositions of the propellant(formula) and the pressures were given.The compositions of the propellant(formula) could be adjusted by giving the burning rates and pressure indexs too.It was of great significance in development of cycle-shortening and cost-saving of solid propellant.
【CateGory Index】: TJ55
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