ZV200P Small Long-Endurance Fuel Hybrid-Wing VTOL UAV, 240 min Endurance, 440 km Range

The ZV200P 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 6660 mm, a fuselage length of 3850 mm, a height of 1262 mm, an empty weight of 85 kg, a maximum takeoff weight of 200 kg, a maximum payload of 70 kg and a fuel tank capacity of 60 L.
The hybrid electric-fuel power system with built-in electric start delivers an endurance of 240 minutes and a maximum range of 440 km.
Its service ceiling reaches 6000 m, with a maximum speed of 150 km/h and a cruise speed of 90-130 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 3420x1100x1100 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.