Description
The ZV12E 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 900 mm, a height of 555 mm, an empty weight of 4.1 kg, a maximum takeoff weight of 12 kg and a maximum payload of 2 kg.
The pure-electric power system with built-in electric start delivers an endurance of 150 minutes and a maximum range of 210 km.
Its service ceiling reaches 5000 m, with a maximum speed of 110 km/h and a cruise speed of 70-100 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 1420x455x400 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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