The JV500 is a medium heavy-payload twin-tail fuel hybrid-wing vertical takeoff and landing (eVTOL) UAV.
It combines electric quad-rotor lift power with a fuel tail-push cruise propeller in a twin-tail hybrid-wing layout, taking off and landing vertically without a runway.
It has a wingspan of 5000 mm, a fuselage length of 2750 mm, an empty weight of 55 kg, a maximum takeoff weight of 135 kg and a maximum payload of 35 kg.
The hybrid electric-fuel power system with built-in electric start delivers an endurance of up to 480 minutes and a maximum range of 1120 km.
Its service ceiling reaches 5000 m, with a maximum speed of 250 km/h and a cruise speed of 140 km/h.
The aircraft withstands level-7 winds, offers an IP55 (customizable) rating and operates from -20°C to +50°C.
The airframe is built of carbon fiber composite for a light yet rugged structure.
Dual GNSS positioning modules, dual IMUs and dual gyroscopes are built into the flight controller for high flight-safety redundancy.
It supports RTK/PPK differential systems with a customizable telemetry range of 15/30/50 km to meet high-precision mission needs.
It is well suited for industrial applications such as heavy payload delivery and long-endurance inspection.


JV500 Medium Heavy-Payload Twin-Tail Fuel Hybrid-Wing UAV, 480 min Endurance, 1120 km Range
The JV500 is a medium heavy-payload twin-tail fuel hybrid-wing eVTOL UAV with electric quad-rotor lift and fuel tail-push cruise propulsion, a 135 kg MTOW, a 35 kg payload, 480 minutes of endurance and a 1120 km range; its carbon fiber airframe and RTK/PPK support make it ideal for heavy payload delivery and long-endurance operations.
Original price was: $76,200.00.$59,400.00Current price is: $59,400.00.
| Product Positioning | Medium Heavy-Payload Twin-Tail Hybrid-Wing |
|---|---|
| Takeoff/Landing Mode | VTOL (Vertical Takeoff & Landing) |
| Power System | Fuel-Powered |
| Start Mode | Built-In Electric Start |
| VTOL Lift Power | Electric Quad-Rotor |
| Cruise Power | Fuel Tail-Push Propeller |
| Wingspan (mm) | 5000 |
| Fuselage Length (mm) | 2750 |
| MTOW (kg) | 135 |
| Empty Weight (kg) | 55 |
| Max Payload (kg) | 35 |
| Endurance | 480 min |
| Max Range (km) | 1120 |
| Service Ceiling (m) | 5000 |
| Max Speed (km/h) | 250 |
| Cruise Speed (km/h) | 140 |
| Wind Resistance | Level 7 |
| IP Rating | IP55 (customizable) |
| Operating Temperature | -20°C to +50°C |
| Airframe Material | Carbon Fiber Composite |
| Redundancy Design | Dual GNSS positioning modules; dual IMUs and dual gyroscopes built into the flight controller |
| Telemetry Range (km) | 15/30/50 km (customizable) |
| Differential System | RTK/PPK |
| Transport Size | 230x93x94cm |
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