The aim of this work is to study the kerosene explosibility in closed or ve
nted vessels and to develop an application to safety systems. The basic cha
racteristics of the model have been developed for the ignition and the comb
ustion of propulsive powders and adapted to liquid fuels with appropriate p
arameters linked to simplified kinetics. A simple representation of the com
bustion phenomena based on energy transfers and the action of specific mole
cular species is presented. The pressure venting, due to the vent breaking
is calculated taking into account the mass rate of discharge of the differe
nt products in the assumption of the standard orifice equations. The model
allows the study of various parameters such as the nature of the kerosene,
the fuel ratio of the mixture, the ignition energy, the thermal exchanges a
nd the influence of the pressure venting or the vent area. The theoretical
results have been compared with data obtained in the course of experiments
performed in small vessel volumes (V-0 = 13 and 33 1) and indicate correct
preliminary tendencies.