Model | T181-500 |
Maximum Deployment Weight | 500 kg |
Maximum Deployment Speed | 220 km/h |
Ejection System Component Weight | 2.2kg |
Ejection System Dimensions | Φ79x306mm |
Parachute Component Weight | 9.3kg |
Packaging Method | Soft Pack |
Container Dimensions | 35x25x15 cm |
Total System Weight | 11.5kg |
Deployment Time (at 90 km/h level flight) | 6 s |
Minimum Deployment Altitude (at 90 km/h level flight) | 100 m |
Maximum Deployment Load | 6g |
Maximum Descent Rate (at 1500 meters standard daytime temperature) | ≤7m/s (equivalent to a fall from a height of 2.5 meters) |
Closure System | yes |
Main Canopy Area | 110 ㎡ |
Total Ejection System Thrust | 400NS |
Rocket Motor Burn Duration | 1±0.1 s |
Rocket Activation Method | Manual Activation |
Operating Temperature Range | – 40°C – +60°C |
Maintenance Interval | 6Years |
System Service Life | 12 Years |
The T181 Aircraft Parachute Recovery System (APRS) utilizes a Mechanical Activation Rocket to provide essential safety for fixed-wing aircraft in emergency situations. When an aircraft faces significant malfunctions or loss of control, the system slows the descent, helping to stabilize the flight and ensuring a controlled and safe landing.
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