T182 Aircraft Emergency Parachute (Electrically Activated Rocket)

Product Details

The T182 Aircraft Parachute Recovery System (APRS) is an advanced emergency safety solution for fixed-wing aircraft, featuring an electrically activated rocket to enable rapid parachute deployment during critical situations. Designed to respond to severe malfunctions or loss of control, the system slows descent, stabilizes the aircraft, and ensures a controlled landing—effectively protecting both crew and equipment.

Equipped with dual deployment options—manual activation and flight control activation—the T182 delivers flexible, reliable recovery capabilities. Its integrated Electronic Control Unit (ECU) supports CAN, UART, and PWM communication protocols, enabling seamless compatibility with various aircraft systems. Engineered to adapt to diverse fixed-wing platforms, it is tailored to meet the specific safety needs of modern aviation.

Model Specifications

T182-350Maximum deployment weight: 350 kgMaximum deployment speed: 220 km/hEjection system component weight: 2.2 kgEjection system dimensions: Φ79x306mmParachute component weight: 7.6 kgPackaging: Soft packContainer dimensions: 30x25x15 cmTotal system weight: 9.8 kgDeployment time (at 90 km/h level flight): 6 sMinimum deployment altitude (at 90 km/h level flight): 90 mMaximum deployment load: 6gMaximum descent rate (1500m, standard daytime temperature): ≤7m/s (equivalent to a 2.5m fall)Closure system: IncludedMain canopy area: 92 ㎡Total ejection system thrust: 400NSRocket motor burn duration: 1±0.1 sRocket activation methods: Manual activation, Flight control activationECU communication protocols: CAN, PWM, RS-232ECU power input: 12-36vOperating temperature range: –40°C to +60°CMaintenance interval: 6 yearsSystem service life: 12 years

T182-500Maximum deployment weight: 500 kgMaximum deployment speed: 220 km/hEjection system component weight: 2.2 kgEjection system dimensions: Φ79x306mmParachute component weight: 9.3 kgPackaging: Soft packContainer dimensions: 35x25x15 cmTotal system weight: 11.5 kgDeployment time (at 90 km/h level flight): 6 sMinimum deployment altitude (at 90 km/h level flight): 100 mMaximum deployment load: 6gMaximum descent rate (1500m, standard daytime temperature): ≤7.5m/s (equivalent to a 2.9m fall)Closure system: IncludedMain canopy area: 110 ㎡Total ejection system thrust: 400NSRocket motor burn duration: 1±0.1 sRocket activation methods: Manual activation, Flight control activationECU communication protocols: CAN, PWM, RS-232ECU power input: 12-36vOperating temperature range: –40°C to +60°CMaintenance interval: 6 yearsSystem service life: 12 years

T182-650Maximum deployment weight: 650 kgMaximum deployment speed: 220 km/hEjection system component weight: 2.5 kgEjection system dimensions: Φ79x355mmParachute component weight: 11.3 kgPackaging: Soft packContainer dimensions: 15×26×50 cmTotal system weight: 13.8 kgDeployment time (at 90 km/h level flight): 6 sMinimum deployment altitude (at 90 km/h level flight): 120 mMaximum deployment load: 6gMaximum descent rate (1500m, standard daytime temperature): ≤7.5m/s (equivalent to a 2.9m fall)Closure system: IncludedMain canopy area: 140㎡Total ejection system thrust: 700NSRocket motor burn duration: 1±0.1 sRocket activation methods: Manual activation, Flight control activationECU communication protocols: CAN, PWM, RS-232ECU power input: 12-36vOperating temperature range: –40°C to +60°CMaintenance interval: 6 yearsSystem service life: 12 years

T182-800Maximum deployment weight: 800 kgMaximum deployment speed: 220 km/hEjection system component weight: 2.5 kgEjection system dimensions: Φ79x355mmParachute component weight: 12.5 kgPackaging: Soft packContainer dimensions: 40×14×34 cmTotal system weight: 15 kgDeployment time (at 90 km/h level flight): 6 sMinimum deployment altitude (at 90 km/h level flight): 140 mMaximum deployment load: 6gMaximum descent rate (1500m, standard daytime temperature): ≤7.5m/s (equivalent to a 2.9m fall)Closure system: IncludedMain canopy area: 175㎡Total ejection system thrust: 700NSRocket motor burn duration: 1±0.1 sRocket activation methods: Manual activation, Flight control activationECU communication protocols: CAN, PWM, RS-232ECU power input: 12-36vOperating temperature range: –40°C to +60°CMaintenance interval: 6 yearsSystem service life: 12 years