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.

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