Description
The JF110 is a small high-performance rapid-response survey UAV.
It is powered by an aviation-kerosene turbojet engine in a fuel tail-push layout with built-in electric start, taking off by assisted boost and recovering by parachute.
It has a wingspan of 1590 mm, a fuselage length of 1600 mm, an empty weight of 12 kg, a maximum takeoff weight of 40 kg and a mission payload of 24.5 kg.
The endurance is 30 minutes and the maximum range is 120 km.
Its service ceiling reaches 5000 m, with a maximum speed of 400 km/h and a cruise speed of 220 km/h.
The aircraft withstands level-7 winds, offers an IPX4 rating and operates from -20°C to +50°C.
The airframe is built of aviation-grade fiberglass for light weight and durability.
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 purpose-built for integrated survey missions.









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