| Model | T192-350 |
| Maximum Deployment Weight | 350 kg |
| Maximum Deployment Speed | 220 km/h |
| Ejection System Component Weight | 2.2kg |
| Ejection System Dimensions | Φ79x306mm |
| Parachute Component Weight | 7.6kg |
| Packaging Method | Soft Pack |
| Container Dimensions | 30x25x15 cm |
| Total System Weight | 9.8kg |
| Deployment Time (under Hovering Conditions) | 3s |
| Minimum Deployment Altitude (under Hovering Conditions) | 40m |
| 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) |
| Main Canopy Area | 92 ㎡ |
| Total Impulse | 400NS |
| Rocket Motor Burn Duration | 1±0.1 s |
| Rocket Activation Method | Manual Activation Flight Control Activation |
| ECU Communication Protocol | CAN \ PWM \ RS-232 |
| ECU Power Input | 12-36v |
| 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.
The T193 Emergency Recovery Parachute System is tailored to fulfill the safety needs of eVTOLs, low-altitude multirotors, and similar aerial vehicles. This state-of-the-art system employs a gas-ejection mechanism for parachute deployment, providing rapid and dependable activation in critical situations. It offers multiple activation modes, including manual operation, flight control system-triggered deployment, and autonomous activation for enhanced operational flexibility.
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