Future Soldier Solution Supplier

The T192 Emergency Recovery Parachute System

The T192 Emergency Recovery Parachute System is a cutting-edge safety solution custom-engineered for eVTOLs, low-altitude multirotors, and other aerial platforms. Its core innovation lies in an electrically triggered micro-rocket deployment mechanism, ensuring fast, reliable parachute activation during emergencies. Supporting both manual activation (giving pilots direct control) and automatic deployment via integration with flight control systems, it addresses the critical need for rapid response in low-altitude vertical takeoff and landing (VTOL) operations. Seamlessly compatible with modern flight control units (ECUs) through CAN, PWM, or RS-232 protocols, the T192 reduces descent speed significantly, enhancing safety for passengers, crew, and equipment during emergency landings.

Product Details

1. Core Design & Operation

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

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

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

2. Key Features & Advantages

· Rapid Deployment: Fast activation (3–4s under hovering conditions) minimizes altitude loss, crucial for low-altitude emergencies.

 

· High Compatibility: Works with diverse eVTOL and multirotor models, thanks to flexible communication protocols and 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 long-term reliability in harsh environments.

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

3. Model-Specific Specifications

Each T192 model is tailored to different platform weights, with shared core features (dual activation, ECU compatibility) and targeted parameters:

· T192-350: Supports a maximum deployment weight of 350kg, with a total system weight of 9.8kg (ejection system: 2.2kg; parachute component: 7.6kg). Packaged in a 30x25x15cm soft pack, it deploys in 3s under hovering conditions, with a minimum deployment altitude of 40m. Maximum descent rate is ≤7 m/s (equivalent to a 2.5m fall), and the main canopy area is 92㎡. It delivers 400NS total impulse with a rocket motor burn duration of 1±0.1s.

· T192-500: Accommodates up to 500kg, with a total system weight of 11.5kg (ejection system: 2.2kg; parachute component: 9.3kg). Packaged in a 35x25x15cm soft pack, deployment takes 3s under hovering, with a minimum altitude of 50m. Maximum descent rate is ≤7.5 m/s (2.9m fall equivalent), and the main canopy spans 110㎡. It shares the 400NS total impulse and 1±0.1s burn duration.

· T192-650: Handles 650kg, with a total system weight of 13.8kg (ejection system: 2.5kg; parachute component: 11.3kg). Packaged in a 15×26×50cm soft pack, deployment takes 4s under hovering, with a minimum altitude of 50m. Maximum descent rate is ≤7.5 m/s (2.9m fall equivalent), and the main canopy area is 140㎡. It delivers 700NS total impulse with a 1±0.1s burn duration. 

·T192-800: Supports up to 800kg, with a total system weight of 15kg (ejection system: 2.5kg; parachute component: 12.5kg). Packaged in a 40×14×34cm soft pack, deployment takes 4s under hovering, with a minimum altitude of 60m. Maximum descent rate is ≤7.5 m/s (2.9m fall equivalent), and the main canopy spans 175㎡. It shares the 700NS total impulse and 1±0.1s burn duration.

· 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

 

 

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