The T191 Emergency Recovery Parachute System is specifically engineered to meet the safety demands of eVTOL, low-altitude multirotors, and other aerial platforms. Its design incorporates a mechanically activated rocket deployment system, ensuring rapid and reliable parachute deployment in critical emergency situations. The system is manually activated, providing the pilot with direct control to respond to power failures, flight malfunctions, or structural issues.
| Model | T191-800 |
| Maximum Deployment Weight | 800kg |
| Maximum Deployment Speed | 110km/h |
| Ejection System Component Weight | 2.5kg |
| Ejection System Dimensions | Φ79x355mm |
| Parachute Component Weight | 12.5kg |
| Packaging Method | Soft Pack |
| Container Dimensions | 40×14×34cm |
| Total System Weight | 15kg |
| Deployment Time (under Hovering Conditions) | 4s |
| Minimum Deployment Altitude (under Hovering Conditions) | 80m |
| Maximum Deployment Load | 6g |
| Maximum Descent Rate (at 1500 meters standard daytime temperature) | ≤7.5m/s (equivalent to a fall from a height of 2.9 meters) |
| Main Canopy Area | 175㎡ |
| Total Impulse | 700NS |
| 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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