T192 Aircraft Emergency Parachute (Electrically Activated Rockets)

Product Details

The T192 Emergency Recovery Parachute System is engineered for eVTOLs, low-altitude multirotors, and urban air mobility (UAM) platforms, combining advanced deployment technology with versatile performance to address critical in-flight emergencies.

1. Core Design & Operation

Electric Micro-Rocket Deployment: Uses an electrically triggered micro-rocket system for forceful, rapid parachute ejection—essential for low-altitude emergencies where split-second timing is critical.

Dual Activation Modes: Pilots can activate manually for direct control, while automatic deployment integrates with onboard flight systems, triggering instantly upon detecting anomalies (e.g., power loss, structural failure).

ECU Compatibility: Seamlessly connects with modern flight control units via CAN, PWM, or RS-232 protocols, accepting 12–36V power input to align with standard aircraft electronics.

2. Key Features & Advantages

Rapid Deployment: Activates in 3–4 seconds under hovering conditions, minimizing altitude loss—vital for low-altitude emergencies.

Broad Compatibility: Works with diverse eVTOL and multirotor models, thanks to flexible communication protocols and universal power input ranges.

Controlled Descent: Low maximum descent rates (≤7–7.5 m/s) reduce impact to levels equivalent to a 2.5–2.9m fall, protecting occupants and equipment.

Extreme Durability: Operates in -40°C to +60°C, with a 12-year service life and 6-year maintenance intervals, ensuring reliability in harsh environments.

Versatile Performance: Handles deployment speeds up to 220 km/h across models, adapting to diverse flight scenarios.

3. Model-Specific Specifications
Each model is tailored to different platform weights, with shared core features (dual activation, ECU compatibility) and targeted parameters:

T192-350Maximum deployment weight: 350kgTotal system weight: 9.8kg (ejection system: 2.2kg; parachute component: 7.6kg)Packaging: 30x25x15cm soft packDeployment time (hovering): 3sMinimum deployment altitude: 40mMaximum descent rate: ≤7 m/s (equivalent to a 2.5m fall)Main canopy area: 92㎡Total impulse: 400NSRocket motor burn duration: 1±0.1s

T192-500Maximum deployment weight: 500kgTotal system weight: 11.5kg (ejection system: 2.2kg; parachute component: 9.3kg)Packaging: 35x25x15cm soft packDeployment time (hovering): 3sMinimum deployment altitude: 50mMaximum descent rate: ≤7.5 m/s (equivalent to a 2.9m fall)Main canopy area: 110㎡Total impulse: 400NSRocket motor burn duration: 1±0.1s

T192-650Maximum deployment weight: 650kgTotal system weight: 13.8kg (ejection system: 2.5kg; parachute component: 11.3kg)Packaging: 15×26×50cm soft packDeployment time (hovering): 4sMinimum deployment altitude: 50mMaximum descent rate: ≤7.5 m/s (equivalent to a 2.9m fall)Main canopy area: 140㎡Total impulse: 700NSRocket motor burn duration: 1±0.1s

T192-800Maximum deployment weight: 800kgTotal system weight: 15kg (ejection system: 2.5kg; parachute component: 12.5kg)Packaging: 40×14×34cm soft packDeployment time (hovering): 4sMinimum deployment altitude: 60mMaximum descent rate: ≤7.5 m/s (equivalent to a 2.9m fall)Main canopy area: 175㎡Total impulse: 700NSRocket motor burn duration: 1±0.1s

All models feature a maximum deployment load of 6g, dual activation (manual/flight control), and operate in -40°C to +60°C.

4. Ideal Applications

eVTOLs (electric vertical takeoff and landing aircraft)

Low-altitude multirotor drones

Urban air mobility (UAM) platforms

Commercial or passenger-carrying aerial vehicles requiring integrated emergency recovery systems