The work was carried out by order of FSUE "GosMKB" Vympel "them.I.I.Toropov, 2002.
In this work, the rocket launch was simulated taking into account the dynamics of the system "aircraft + airplane catapult mechanism + rocket + external environment".The main features of the model: an elastic model of the construction of catapult levers; elastic model of the rocket design;the impact of aerodynamic forces on the aircraft, rocket and catapult levers;the mutual influence of the dynamics of the movement of the aircraft and the rocket.