FIELD: flight vehicles.
SUBSTANCE: invention relates to the aircraft anti-spin parachute systems. The said system contains parachute (5) and shroud lines (6), outer container (1) fastened onto the aircraft and equipped with detachable tail cone (2) incorporating a pyrotechnic mechanism. The tail cone is connected with inner container (4) housing the laid parachute to which the end of cords (6) are connected, the other ends of the said cords being connected to the outer container by means of lock (7) retaining and releasing the cords. Second lock (10) retains tail cone (2) against outer container (1) in a normal flight conditions. The outer container can be made suspended or built-in the aircraft tail girder.
EFFECT: smaller time of the parachute opening.
3 cl, 3 dwg
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