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COMMERCIAL AIRCRAFT

Feiyu VT04

By Feiyu ↗

The Feiyu VT04 is a modular vertical-takeoff fixed-wing UAV for mapping, inspection, reconnaissance and payload missions. Its composite airframe provides internal integration space and quick-release payload attachment, with propulsion and an FPV gimbal camera supplied as standard. Maximum payload is 3 kg; endurance depends on load, with differing stated duration figures.

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FY-VT04 fixed-wing UAV with four lift rotors and a rear propeller.
FY-VT04 fixed-wing UAV with four lift rotors and a rear propeller.
Maximum payload3 kg
Maximum takeoff weight13.5 kg
Maximum flight endurance240 minutes; 120 minutes carrying 1.5 kgEndurance depends on payload; 120 minutes with a 1.5 kg payload.
Wingspan2500 mm
Aircraft configurationVertical-takeoff fixed-wing UAVVT04 model
Aircraft type and propulsion layout4+1 vertical-takeoff-and-landing fixed-wing UAV

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

SpecificationValue & conditions
Aircraft configurationVertical-takeoff fixed-wing UAVVT04 model
Aircraft type and propulsion layout4+1 vertical-takeoff-and-landing fixed-wing UAV
Airframe materialsCarbon fiber, fiberglass and Kevlar
Takeoff and landingVertical takeoff and landing
Length1260 mm
Wingspan2500 mm
Maximum flight endurance240 minutes; 120 minutes carrying 1.5 kgEndurance depends on payload; 120 minutes with a 1.5 kg payload.
Maximum payload3 kg
Standard payload1.5 kg
Maximum takeoff weight13.5 kg
Cruising speed75–144 km/h
Wind resistanceGreater than force 6
Headwind resistanceGreater than force 6Headwind.
Maximum operating altitude4800 m
Operating temperature range−20°C to 50°C
Transport case dimensions1470 mm × 560 mm × 400 mm
Included equipmentHigh-performance propulsion and an FPV gimbal cameraStandard supplied configuration.
Modular constructionQuickly detachable fuselage and wings; disassembled components fit in a dedicated aviation case
Deployment timeReady for takeoff within 5 minutesThree-step assembly; no calibration required.
Rain protectionWhole-airframe rain protection
Payload integration spaceReserved internal cabin space for different cameras and payloads up to 3 kg
Payload equipment optionsOrthographic imaging camera, oblique five-lens camera, gas-detection pod, 30× visible-light pod, and infrared dual-/triple-sensor pods
CustomizationOEM/ODM customization supported
Automated survey flightAutomatic route generation with photography at fixed points or distance intervals
Point-directed flightPoint-directed flight followed by circling and target lockFixed-wing flight to the target point.
Payload attachmentQuick-release pod attachment
Headline endurance figure220 minutes maximum endurance, marked with an asterisk
Additional endurance figure140 minutes; optimal payload stated as 1.5 kgPresented alongside an optimal payload of 1.5 kg, without an explicit endurance test configuration.
Intended applicationsTerrain mapping, border reconnaissance, power-line inspection, drought and flood assessment, forest-fire detection, firefighting and disaster relief, and targeted airdrops
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