The TX-140L is a long-range unmanned aircraft designed for heavy-payload missions, extended flight time, and complex deployment scenarios.
Supporting rocket-assisted launch, vehicle-based launch, and standard catapult deployment, it can adapt to diverse operational environments.
With a maximum payload of 50 kg, 6-hour endurance, and up to 1000 km range, the TX-140L is suitable for deep-strike missions, long-distance delivery, and extended reconnaissance tasks.
Its low-RCS aerodynamic design enables high concealment and reduced detectability, while the aviation-grade carbon fiber structure ensures high strength and light weight.
Engineered for large-scale deployment and saturated launch missions, the TX-140L offers low maintenance cost, high reliability, and flexible application across military and special-purpose operations.
Technical Specifications
| Parameter | Value |
|---|---|
| MTOW (Max Take-off Weight) | 150 kg |
| Payload Capacity | 50 kg (Payload + fuel) |
| Endurance (Fight Time) | 6 h |
| Max Range | 1000 km |
| Length | 2480 mm |
| Height | 425 mm |
| Wingspan | 2150 mm |
| Airframe Material | Aviation carbon fiber composites |
| Engine | Gasoline engine |
| Safe Flight Speed | 40–65 m/s |
| Cruising Speed | 50 m/s |
| Diving Speed | 58 m/s |
| Fuel Consumption | 10 L/h |
| Operating Altitude | 4000 m |
| Operating Temperature | -20°C ~ +55°C |
| Wind Resistance | Take-off: Level 5 / Flight: Level 6 (8.0–10.7 m/s take-off, 10.8–13.8 m/s cruising) |
| Launch Method | Rocket booster / Vehicle takeoff |











