Fixed-Wing VTOL UAV
Our Fixed-Wing VTOL UAV series is built for missions that require both flexible takeoff and efficient long-range flight. Combining vertical takeoff and landing with fixed-wing cruise efficiency, the platform can operate without a runway while covering large areas with lower energy use. With payload capacities from 1.5 kg to 80 kg, it supports surveillance, mapping, inspection, emergency response, communication relay, and other multi-mission applications.
Designed for practical field deployment, the Fixed-Wing VTOL UAV platform is available in both electric and fuel-powered configurations. It offers stable performance, flexible payload integration, and dependable operation in demanding environments.
| Parameter |
XF-200
|
HQ-600
|
Q13
|
Q20
|
Q32
|
Q40
|
Q50
|
Q80
|
Q150
|
|---|---|---|---|---|---|---|---|---|---|
| Type | Patrol UAV | VTOL Fixed-Wing UAV | VTOL Fixed-Wing UAV | VTOL Fixed-Wing UAV | VTOL Fixed-Wing UAV | VTOL Fixed-Wing UAV | VTOL Fixed-Wing UAV | VTOL Fixed-Wing UAV | Fixed-Wing UAV |
| Wingspan | 2.95 m | 6.235 m | 2.25 m | 3.35 m | 4.0 m | 4.8 m | 4.8 m | 7.0 m | 8.5 m |
| Length | 3.2 m | 4.08 m | 1.4 m | 1.85 m | 2.1 m | 2.6 m | 2.6 m | 3.8 m | 5.3 m |
| Maximum Takeoff Weight | 200 kg | 155 kg | 13 kg | 18 kg | 30 kg | 60 kg | 55 kg | 180 kg | 280 kg |
| Standard Payload | 50 kg | 45 kg | 1.5 kg | 3 kg | 5 kg | 15 kg | 15 kg | 40 kg | 80 kg |
| Endurance | >6 h (with 50 kg payload) | 12 h | 3 h (no payload) | 3 h (with 1 kg payload) | 3 h (no payload) | 3 h (no payload) | 8 h | 8 h | 12 h |
| Cruise Speed | 180–200 km/h | 110–150 km/h | 18–30 m/s | 18–30 m/s | 22–36 m/s | 25–36 m/s | 25–36 m/s | 120–150 km/h | 140–160 km/h |
| Maximum Flight Speed | 250 km/h | 190 km/h | 35 m/s | 40 m/s | 40 m/s | 40 m/s | 40 m/s | 160 km/h | 200 km/h |
| Maximum Flight Altitude | 3000 m | 5000 m | <5000 m | — | <5000 m | <5000 m | <5000 m | ≤4000 m | ≤6000 m |
| Communication / Control Range | Standard 50 km integrated data link (optional 100 km) | Maximum control range 50 km | Standard 30 km | Control radius 30 km | Standard 30 km integrated data link (optional 50 km) | Standard 50 km integrated data link (optional 100 km) | Standard 50 km integrated data link (optional 100 km) | Standard 150 km integrated data link | Standard 150 km integrated data link |
| Communication Frequency | 1.4 GHz | — | 1.4 GHz | — | 1.4 GHz | 1.4 GHz | 1.4 GHz | 1.4 GHz | 1.4 GHz |
| Environment / Wind Resistance | — | Max wind resistance: Level 6 | Operating temperature: -20°C to 45°C; Max wind resistance: Level 6 | Max wind resistance: Level 6 | Operating temperature: -20°C to 45°C; Max wind resistance: Level 6 | Operating temperature: -20°C to 45°C; Max wind resistance: Level 6 | — | Operating temperature: -20°C to 45°C; Max wind resistance: Level 6 | Operating temperature: -20°C to 45°C; Max wind resistance: Level 6 |
| Power System | 95# gasoline (mixed oil); 550–600CC two-stroke engine | — | — | — | — | — | 95# gasoline (mixed oil); 10.0 hp; optional 400/800W generator; 120cc two-stroke EFI integrated-start engine | — | — |
| Additional Notes | Suitable for heavy-payload patrol missions, with strong payload capacity, fuel power, and long endurance. | The image also indicates a maximum fuel capacity of 50 L, expandable to 70 L. | Designed for long endurance, modular deployment, high reliability, and fast mission readiness, with support for various payload configurations. | Features a twin-boom inverted V-tail layout and rear pusher propulsion design, with a maximum payload of 3 kg. | A multi-purpose electric UAV with a twin-boom inverted V-tail layout and rear pusher propulsion design. | Offers VTOL capability and heavy-payload performance, with flexible payload integration for different mission needs. | A heavy-payload, long-endurance multi-purpose UAV with a twin-boom inverted V-tail layout. | Mainly designed for emergency communications, inspection, and search-and-rescue missions, and can carry satellite communication antennas and 4G/5G base stations. | Features a high-performance aerodynamic design and composite airframe, and supports payloads such as EO gimbals, communication devices, navigation equipment, small SAR systems, oblique cameras, and laser payloads. |