Simplified Burn-Rate Model for CMDB Propellants
Keywords: RDX, CMDB
AbstractA single model has been proposed to predict the burning rates of bimodal AP,RDX and aluminum containing CMDB propellants. This is done in terms of the respective physical constants on the basis of a recently developed model of combustion of CMDB propellants. The study has been carried out to examine the effects of changes in propellants composition, AP particle size and pressures on burning rate. Computer programs were developed for this purpose and the results obtained for typical sets of input data have been presented and compared with the actual results.
How to Cite
KulkarniA., BhatV., PhadkeS., & NairR. (2013). Simplified Burn-Rate Model for CMDB Propellants. Defence Science Journal, 40(3), 255-262. https://doi.org/10.14429/dsj.40.4467
Armaments & Explosives
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