FIELD: sport.
SUBSTANCE: group of inventions relates to rescue parachute systems. Disclosed system comprises canopy/canopies of main parachute, pilot and brake parachutes. Parachute system is arranged at fuselage tail in two successive controlled cowls. Halyards of main parachute are laid on surface of fuselage with a temporary breakable fastener and are fixed to three points of airframe. Halyards of pilot chute are controlled by an additional intermediate attachment. In compartment or in capsule of main canopy/canopies there is additional brake parachute. Controlled additional attachment of halyard of pilot parachute is made up of branch halyard equipped with guillotine, and has actuation lock. Main canopy has corrugation, provided with guillotine.
EFFECT: group of inventions is aimed at preventing tangling in rear horizontal tail.
9 cl, 1 dwg
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