Description
The ZV13E is a small long-endurance vertical takeoff and landing (eVTOL) fixed-wing UAV.
It combines electric quad-rotor lift power with an electric tail-push cruise propeller in a hybrid-wing layout, taking off and landing vertically without a runway.
It has a wingspan of 2500 mm, a fuselage length of 1560 mm, a height of 345 mm, an empty weight of 3.9 kg, a maximum takeoff weight of 13.5 kg and a maximum payload of 2 kg.
The pure-electric power system with built-in electric start delivers an endurance of 210 minutes and a maximum range of 270 km.
Its service ceiling reaches 5000 m, with a maximum speed of 100 km/h and a cruise speed of 75-79 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 1260x486x405 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 industrial applications such as surveying, inspection and payload delivery.
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