The TX-40F is a high-speed unmanned aircraft designed for rapid penetration missions and flexible deployment across multiple platforms.
Equipped with a pneumatic catapult launch system, it offers low-cost, low-noise, and high concealment performance suitable for fast-response operations.
Its turbojet power system enables flight speeds up to 110 m/s, making it ideal for high-speed breakthrough tasks.
The aircraft supports parachute-based recovery, reducing landing risks and ensuring reusable operation even in complex scenarios.
Constructed with aviation-grade carbon fiber composites, the TX-40F combines low weight with high durability.
With reliable performance, low maintenance cost, and strong environmental adaptability, it is well-suited for large-scale deployments and saturated launch missions.
Technical Specifications
| Parameter | Value |
|---|---|
| MTOW (Max Take-off Weight) | 40 kg |
| Payload | ≥ 7 kg |
| Max Speed | 110 m/s |
| Max Range | 120 km |
| Length | 2100 mm |
| Height | 642 mm |
| Wingspan | 1464 mm |
| Airframe Material | Aviation carbon fiber composites |
| Load (Payload + Fuel) | ≥ 22 kg |
| Safe Flight Speed | 48–110 m/s |
| Cruising Speed | 70 m/s |
| Fuel Consumption | 620 g/min |
| Operating Altitude | ≥ 7000 m |
| Operating Temperature | -20°C ~ +45°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) |
| Take-off Method | Pneumatic catapult |











