FIELD: aviation. SUBSTANCE: flying vehicle is provided with two parachutes. Each parachute is deployed by means of rocket secured after parachute canopy by means of coupling destroyed under action of impact load arising at moment of heaving in the line point of its securing. First, parachute is brought to horizontal position and after cancelling horizontal velocity, parachute is brought to vertical position. After separation of rocket, parachute deployed in horizontal direction is retracted first and then parachute deployed in vertical direction is retracted. EFFECT: enhanced efficiency of deceleration; comfort landing for passengers. 2 cl, 1 dwg
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