This paper contains a description of a shock wave (called a flame when the deflagration is considered)
propagation pattern impact on a motion of a barrier. Here, the numerical research was conducted on a model of
a pyrotechnic actuator, hence, the piston is understood as a movable barrier. The processes occurring within the
pyrotechnic actuators after ignition of a pyrotechnic propellants have been explained. The investigations are
focused on the dependence of a shape of the actuator’s combustion chamber and the piston stroke time. It appears
that the appropriate design of the combustion chamber can decrease the time required for a piston total stroke
using this same type of a propellant. The visualization of the flame occurring due to ignition of the propellant is
crucial for understanding the dependence between the construction of the actuators interior and the piston stroke
time. Therefore, the approach of simulating numerically the flames aroused. The simulation was conducted on
a full scale 3D model of a pyrotechnic actuator which is a detail representation of a real object on which the
verification test will be conducted. However, only the flame propagation was considered here. The material of an
actuators members was not investigated, hence the AUTODYN solver considered them as a single rigid bodies with
its own mass and inertia.
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