Equipped with a variety of task development ability
HC-141 adopts high performance aerodynamic shape design and composite fuselage, which can be widely used in emergency communication, emergency disaster relief, sea area monitoring, magnetic submarine detection, meteorological detection, target detection and identification, etc. The system configuration is flexible, easy to disassemble and assemble, and transition deployment can be rapidly completed according to mission needs.
12h endurance
50kg payload
Wind resistance level 7
Real-time data transmission
Air-cooled, two-cylinder, horizontally-opposed, two-stroke, direct-drive aeroengine, super power to meet the needs of UAV climb, providing stable power guarantee for the entire flight mission system.
The HC-141 is equipped with a 40L fuel tank and has a flight duration of up to 12 hours
fuel tank capacity
flight duration
Fuel composition
Its internal integrated flight control computer and micro-combined navigation system (GPS/INS) can realize one-click automatic takeoff, landing, hovering, return, fixed height, autonomous landing and other forms of autonomous cruise according to the scheduled route.
Automatic take-off and landing & route planning
Automatic flight beyond visual range
Control the attitude of the aircraft
Switch flight mode online
Intelligent control software makes software more convenient
Intelligent control software makes software more convenient