The ZV80P is a small long-endurance 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 hybrid-wing layout, taking off and landing vertically without a runway.
It has a wingspan of 4800 mm, a fuselage length of 2580 mm, a height of 795 mm, an empty weight of 41 kg, a maximum takeoff weight of 90 kg, a maximum payload of 30 kg (including fuel) and a fuel tank capacity of 25 L.
The hybrid electric-fuel power system with built-in electric start delivers an endurance of 360 minutes and a maximum range of 660 km.
Its service ceiling reaches 6000 m, with a maximum speed of 150 km/h and a cruise speed of 100-120 km/h.
The climb rate is <=3.5 m/s and the descent rate is <=1.5 m/s.
It withstands level-5 winds in the VTOL phase and level-6 winds in the cruise phase, with an IP54 rating and an operating temperature range of -10°C to +45°C.
The airframe is built of fiberglass composite for durability.
The airframe stows to 1950x920x710 mm for easy transport and rapid deployment.
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 applications such as heavy payload delivery and long-endurance inspection.



ZV80P Small Long-Endurance Fuel Hybrid-Wing VTOL UAV, 360 min Endurance, 660 km Range
The ZV80P is a small long-endurance fuel hybrid-wing eVTOL UAV with electric quad-rotor lift and fuel tail-push cruise propulsion, a 90 kg MTOW, a 30 kg payload (including fuel) and a 25 L fuel tank, 360 minutes of endurance and a 660 km range; its fiberglass composite airframe and RTK/PPK support make it ideal for heavy-payload delivery and long-endurance operations.
Original price was: $41,700.00.$32,500.00Current price is: $32,500.00.
| Product Positioning | Small Long-Endurance |
|---|---|
| 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) | 4800 |
| Fuselage Length (mm) | 2580 |
| Height (mm) | 795 |
| MTOW (kg) | 90 |
| Empty Weight (kg) | 41 |
| Max Payload (kg) | 30 (incl. fuel) |
| Fuel Tank Capacity (L) | 25 |
| Endurance | 360 min |
| Max Range (km) | 660 |
| Service Ceiling (m) | 6000 |
| Max Speed (km/h) | 150 |
| Cruise Speed (km/h) | 100-120 |
| Climb Rate (m/s) | <=3.5 |
| Descent Rate (m/s) | <=1.5 |
| Wind Resistance | Level 5 (VTOL Phase) / Level 6 (Cruise Phase) |
| IP Rating | IP54 |
| Operating Temperature | -10°C to +45°C |
| Airframe Material | Fiberglass 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 |
| Stowed Size (mm) | 1950x920x710 |
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