Product overview
The Feiyu VT04 combines a 4+1 propulsion layout with a fixed wing and vertical takeoff and landing, removing the need for a runway. Its 1260 mm fuselage and 2500 mm wingspan use carbon fiber, fiberglass and Kevlar. The modular fuselage and wings detach for transport in a 1470 × 560 × 400 mm case. Three-step assembly supports takeoff within five minutes without calibration. The supplied configuration includes high-performance propulsion and an FPV gimbal camera.
Reserved cabin space and quick-release pod attachment support mission-specific equipment, including mapping cameras, gas-detection pods and visible-light or infrared imaging pods. Maximum payload is 3 kg, standard payload is 1.5 kg, and maximum takeoff weight is 13.5 kg. Cruising speed is 75–144 km/h, with a maximum operating altitude of 4800 m and a stated temperature range of −20°C to 50°C. Endurance figures differ: technical specifications give 240 minutes maximum and 120 minutes carrying 1.5 kg; separate figures give 220 and 140 minutes.
Specifications
| Specification | Value & conditions |
|---|---|
| Aircraft configuration | Vertical-takeoff fixed-wing UAVVT04 model |
| Aircraft type and propulsion layout | 4+1 vertical-takeoff-and-landing fixed-wing UAV |
| Airframe materials | Carbon fiber, fiberglass and Kevlar |
| Takeoff and landing | Vertical takeoff and landing |
| Length | 1260 mm |
| Wingspan | 2500 mm |
| Maximum flight endurance | 240 minutes; 120 minutes carrying 1.5 kgEndurance depends on payload; 120 minutes with a 1.5 kg payload. |
| Maximum payload | 3 kg |
| Standard payload | 1.5 kg |
| Maximum takeoff weight | 13.5 kg |
| Cruising speed | 75–144 km/h |
| Wind resistance | Greater than force 6 |
| Headwind resistance | Greater than force 6Headwind. |
| Maximum operating altitude | 4800 m |
| Operating temperature range | −20°C to 50°C |
| Transport case dimensions | 1470 mm × 560 mm × 400 mm |
| Included equipment | High-performance propulsion and an FPV gimbal cameraStandard supplied configuration. |
| Modular construction | Quickly detachable fuselage and wings; disassembled components fit in a dedicated aviation case |
| Deployment time | Ready for takeoff within 5 minutesThree-step assembly; no calibration required. |
| Rain protection | Whole-airframe rain protection |
| Payload integration space | Reserved internal cabin space for different cameras and payloads up to 3 kg |
| Payload equipment options | Orthographic imaging camera, oblique five-lens camera, gas-detection pod, 30× visible-light pod, and infrared dual-/triple-sensor pods |
| Customization | OEM/ODM customization supported |
| Automated survey flight | Automatic route generation with photography at fixed points or distance intervals |
| Point-directed flight | Point-directed flight followed by circling and target lockFixed-wing flight to the target point. |
| Payload attachment | Quick-release pod attachment |
| Headline endurance figure | 220 minutes maximum endurance, marked with an asterisk |
| Additional endurance figure | 140 minutes; optimal payload stated as 1.5 kgPresented alongside an optimal payload of 1.5 kg, without an explicit endurance test configuration. |
| Intended applications | Terrain mapping, border reconnaissance, power-line inspection, drought and flood assessment, forest-fire detection, firefighting and disaster relief, and targeted airdrops |
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