Designed for efficient operation
HC-260 unmanned helicopter adopts the traditional single-rotor helicopter layout, the tail rotor is driven by motor directly, the main rotor is driven by a fuel engine, and the airborne equipment is powered by an integrated generator and battery. The rotor control structure has the same principle as the traditional helicopter, showing excellent flight performance, including high stability and maneuverability. Compared to multi-rotor, the propeller efficiency is higher and the endurance is longer. Support beyond visual range flight, in the case of signal relay can cope with complex geographical environment tasks, such as low altitude operations in mountains 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, circling around, 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