Abstract
This article presents a theoretical model to calculate and solve the problem of the motion of decoy for torpedoes, which arrange in the missile. The missile is decreased speed by parachute with double deployment method. The trajectory of the missile is divided into stages, on each stage different forces act on the missile. At each stage, the motion of the missile is determined by a system of differential equations. The system of differential equations is solved for each stage of the trajectory. The results of the calculation allow determining the appropriate time to activate the drogue and main parachutes to ensure the required speed of the missile when it hits the water and ensures the minimum flight time to increase the efficiency of missiles.
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