T181 Aircraft Emergency Parachute (Mechanical Activation Rocket)

Product Details

The T181 Aircraft Parachute Recovery System (APRS) is an emergency parachute system for fixed-wing aircraft, utilizing a mechanical activation rocket to provide critical safety during emergencies. When an aircraft suffers severe malfunctions or loss of control, the system slows descent, stabilizes flight, and enables a controlled, safe landing.

Equipped with ballistic ejection deployment and an electrically initiated solid-fuel small rocket for autonomous flight control activation, it relies primarily on manual activation—ensuring reliable recovery in critical scenarios. By reducing descent speed and enabling dependable recovery, it minimizes risks of aircraft damage and crew injury, with designs tailored to various fixed-wing platforms.

Product Description
In an emergency, pilots activate a towing rocket (manually or automatically), which extracts the canopy. Rapid inflation controls the aircraft’s descent speed, guiding it to a steady ground landing—this is the core operation of the emergency recovery system.

Product Features

Compact and lightweight design

Fast parachute opening time

Low opening overload

High inflation reliability

Strong stability during descent

Low stable descent speed

Model Specifications

T181-350Maximum 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: ManualOperating temperature range: –40°C to +60°CMaintenance interval: 6 yearsSystem service life: 12 years

T181-500Maximum 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: ManualOperating temperature range: –40°C to +60°CMaintenance interval: 6 yearsSystem service life: 12 years

T181-650Maximum 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: ManualOperating temperature range: –40°C to +60°CMaintenance interval: 6 yearsSystem service life: 12 years

T181-800Maximum 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: ManualOperating temperature range: –40°C to +60°CMaintenance interval: 6 yearsSystem service life: 12 years