ZV40P Small Long-Endurance Fuel Hybrid-Wing VTOL UAV, 720 min Endurance, 1320 km Range

The ZV40P 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 3700 mm, a fuselage length of 2180 mm, a height of 690 mm, an empty weight of 20 kg, a maximum takeoff weight of 40 kg, a maximum payload of 5 kg and a fuel tank capacity of 14 L.
The hybrid electric-fuel power system with built-in electric start delivers an endurance of up to 720 minutes and a maximum range of 1320 km.
Its service ceiling reaches 6000 m, with a maximum speed of 130 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 1740x740x760 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 ultra-long-endurance inspection and reconnaissance.