ZV55P Small Long-Endurance Fuel Hybrid-Wing VTOL UAV, 240 min Endurance, 460 km Range

The ZV55P is a small long-endurance fuel hybrid-wing vertical takeoff and landing (eVTOL) UAV.
It combines electric quad-rotor lift power with a fuel front-tractor cruise propeller in a hybrid-wing layout, taking off and landing vertically without a runway.
It has a wingspan of 5000 mm, a fuselage length of 3480 mm, a height of 720 mm, an empty weight of 25 kg, a maximum takeoff weight of 55 kg, a maximum payload of 15 kg and a fuel tank capacity of 20 L.
The hybrid electric-fuel power system with built-in electric start delivers an endurance of 240 minutes and a maximum range of 460 km.
Its service ceiling reaches 5000 m, with a maximum speed of 180 km/h and a cruise speed of 90-140 km/h.
The climb rate is <=3.5 m/s and the descent rate is <=1.5 m/s.
The aircraft withstands level-6 winds, offers an IP54 rating and operates from -10°C to +45°C.
The airframe is built of fiberglass composite for durability.
The airframe stows to 3240x680x750 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 payload delivery and long-endurance inspection.