JF110 Small High-Performance Rapid-Response Survey UAV, Turbojet Power, 400 km/h Max Speed

The JF110 is a small high-performance rapid-response survey UAV with an aviation-kerosene turbojet engine in a fuel tail-push layout, a 40 kg MTOW, a 24.5 kg mission payload, 30 minutes of endurance and a 120 km range; it reaches 400 km/h with a service ceiling of 5000 m and withstands level-7 winds, making it ideal for survey missions.

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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.

Additional information

Product Positioning

Small High-Performance Rapid-Response Survey UAV

Takeoff/Landing Mode

Boosted Launch, Parachute Recovery

Power System

Kerosene Turbojet Engine

Start Mode

Built-In Electric Start

Cruise Power

Fuel Tail-Push Propeller

Wingspan (mm)

1590

Fuselage Length (mm)

1600

MTOW (kg)

40

Empty Weight (kg)

12

Max Payload (kg)

24.5

Endurance

30 min

Max Range (km)

120

Service Ceiling (m)

5000

Max Speed (km/h)

400

Cruise Speed (km/h)

220

Wind Resistance

Level 7

IP Rating

IPX4

Operating Temperature

-20°C to +50°C

Airframe Material

Aviation-Grade Fiberglass

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

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