BRAKE PARACHUTE PTK-29

The parachute system is deployed by the pilot after touching the runway by the main wheels of the aircraft. At the moment the cap is released of releasing the cap from the parachute container of the aircraft, the cone spring of the exhaust parachute straightens and enables the second exhaust parachute, which extracts the main parachute of its camera. Inflated main parachute resists aircraft movement and reduces the length of its run along the runway. The system provides speed suppression of an aircraft during landing and is deployed at velocity not less than 180 km/h and up to 300 km/h.

SPACIFICATIONS

The maximum operating load does not exceed
Rmax 61656 H (6285 Krc)
Overall dimensions of the parachute system in the folded state:

Diameter
0,17 m
Height
0,7 m
Parachute system weight, not more than
8 kg
Service time, including shelf-life
8 years
Resource of the parachute system
40 applications
Time of laying the parachute system:

with the press for more than
10 minutes
manually no more than
20 minutes
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