Designed for efficient operation
HC-260 unmanned helicopter adopts the traditional single-rotor helicopter layout, the tail rotor is directly driven by motor, the main rotor is driven by a fuel engine, and the airborne equipment is powered by an integrated generator and battery. The rotor control system operates on the same principles as a traditional helicopter, delivering excellent flight performance, including high stability and maneuverability. Compared to multi-rotor, the propeller efficiency is higher and the endurance is longer. It supports beyond visual range flight and, with the aid of signal relay, can perform tasks in complex geographical environments, such as low-altitude operations in mountainous regions and over the sea.
75kg payload
Universal platform for multiple payloads
Endurance 120min@55kg
Multiple application scenarios
HC-260 supports using aviation kerosene fuel
70L
210cc twin-engine
92# gasoline/aviation kerosene
The flight control system integrates the flight control computer and the micro-integrated navigation system (GPS/INS), which has the functions of one-click automatic take-off, landing, hovering, loitering, returning, fixed-height, opening parachute and various forms of autonomous cruise according to the scheduled route.
Autonomous takeoff and landing & route planning
Automatic flight beyond visual range
Control the attitude of the aircraft
Switch flight mode online
Empowering flight operations with unlimited potential
Empowering flight operations with unlimited potential