Abstract
In this study, the six-lump model was sufficient to describe the kinetics of vacuum gas oil (VGO) hydrocracking to produce aviation turbine kerosene (ATK). The model aim was to test various operating parameters on maximizing the ATK yields. These parameters were temperature, pressure, catalyst deactivation, residence time, and reaction rate order. Temperature and pressure increase were in favor of increase ATK yields. Residence time had an optimum value that was around 0.5 h after which no increase of ATK yield was observed. Increasing reaction rate order of VGO increased ATK yields.
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