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EN
Monolithic nitrocellulose and cellulose (NC-C) composites solidified with starch were used in a model reactive armour with steel plates. The acceleration ability of the gaseous reaction products of composites was examined by the use of X-ray technique. The effectiveness of the reactive armour containing NC-C composites in weakening the ability of jet penetration was assessed experimentally on the basis of the size of holes in the steel plates and effects of the impact of jet particles on a steel plate located under the armour. It has been shown that the size of the holes in the driven plate increases and the degree of penetration of the “witness” plate is reduced with the decrease of the angle of jet impact. The modified Gurney model was applied to simulate the process of driving steel plates in the reactive armor with a layer of NC-C composite. The model was verified by using the results of X-ray recording of plates driven by the reaction products. The effectiveness of reactive armors with NC-C composites in weakening the penetration ability of shaped charge jets was evaluated in a manner based on the results of theoretical modeling
EN
Monolithic nitrocellulose and cellulose composites (NC-C) were obtained by cross-linking a mixture of nitrocellulose with cellulose using hexamethylene diisocyanate (HDI). They were incorporated into a model reactive armour. An X-ray technique was used to examine the infuence of the cellulose content on the accelerating ability of the gaseous reaction products of the composites. The modifed Gurney model was used to simulate the process of driving steel plates in the reactive armour after jet impact. Formulae for the determination of the time-space characteristics of the plates’ movement were derived. The results of the X-ray recording of the plates driven by the explosion products of monolithic nitrocellulose and cellulose composites (NC-C) were used for the verifcation of the model.
EN
Monolithic nitrocellulose-cellulose composites were prepared by separately cross-linking the mixed precursors (NC + C) with hexamethylene diisocyanate (HDI). The syntheses were optimised according to the component mass ratios, HDI, solvent and catalyst concentration. The concentrations of the reactants and cure catalyst are the most important factors. The general method of synthesis involved dissolving HDI and the catalyst in methylene chloride and then wetting an NC-C mixture with the solution. The resulting mixture was placed in a sealed box for cross-linking at room temperature. Finally the solvent was evaporated at ca. 40 C. The NC-C composites obtained were characterized using TG/DTA and sensitivity to friction and drop weight impact, and were used as energetic materials in reactive armour elements.
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