ZV15E Small Long-Endurance VTOL Fixed-Wing UAV, 210 min Endurance, 280 km Range

Description

The ZV15E 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 2600 mm, a fuselage length of 1500 mm, a height of 600 mm, an empty weight of 4.7 kg, a maximum takeoff weight of 15 kg and a maximum payload of 2.5 kg.
The pure-electric power system with built-in electric start delivers an endurance of 210 minutes and a maximum range of 280 km.
Its service ceiling reaches 5000 m, with a maximum speed of 100 km/h and a cruise speed of 70-90 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 1530x430x585 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.

Additional information

Product Positioning	Small Long-Endurance
Takeoff/Landing Mode	VTOL (Vertical Takeoff & Landing)
Power System	Pure Electric
Start Mode	Built-In Electric Start
VTOL Lift Power	Electric Quad-Rotor
Cruise Power	Electric Tail-Push Propeller
Wingspan (mm)	2600
Fuselage Length (mm)	1500
Height (mm)	600
MTOW (kg)	15
Empty Weight (kg)	4.7
Max Payload (kg)	2.5
Endurance	210 min
Max Range (km)	280
Service Ceiling (m)	5000
Max Speed (km/h)	100
Cruise Speed (km/h)	70-90
Climb Rate (m/s)	<=3.5
Descent Rate (m/s)	<=1.5
Wind Resistance	Level 6
IP Rating	IP54
Operating Temperature	-10°C to +45°C
Airframe Material	Fiberglass Composite
Redundancy Design	Dual GNSS positioning modules; dual IMUs and dual gyroscopes built into the flight controller
Telemetry Range (km)	15/30/50 km (customizable)
Differential System	RTK/PPK
Stowed Size (mm)	1530x430x585

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