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.Current price is: $32,500.00.

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.

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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