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Aviation quality, keep improving
HC-140 fixed wing UAV is made of carbon fiber composite material, which has the characteristics of large load, stable flight, easy operation, long endurance and high flight efficiency, and can be used for border patrol, forest fire prevention, nuclear radiation monitoring, pipeline inspection, material delivery, flight training and other tasks.
Max payload 35kg
Max endurance 6h
Easy to operate
fully autonomous takeoff and landing by running
Two cylinders are horizontally opposed, air-cooled, two-stroke, electronic injection system, mixed lubrication
Honeycomb Aerospace UAV with photoelectric camera can be used in inspection, security and emergency search and rescue and other scenarios, the camera integrates high-resolution infrared camera, 30x high-definition visible light camera and the longest measurement range of 5km laser rangefinder, as well as gyro-stabilized platform, with visible and infrared real-time video return, point of interest and target positioning, close observation and the ability to work all day.
Honeycomb Aerospace UAV with photoelectric camera can be used in inspection, security and emergency search and rescue and other scenarios. Two-axis three-lens target positioning camera, integrated with a 30x optical zoom visible light camera, a 640×512 high-resolution infrared camera, the farthest measurement range of 3km laser rangefinder, as well as high-precision gyro-stablized platform, with the ability to work all day.
Honeycomb Aerospace UAV with an airborne high-performance base station can provide users with high-speed broadband wireless Internet access, which is used in emergency rescue and post-disaster communication recovery. The base station has a simple and compact design with low power consumption.
The loads of Honeycomb Aerospace UAVs support third-party customization
HC-140 is equipped with a 30L large fuel tank, the engine has a high fuel efficiency, and can fly 650km
Tank capacity
flight time
Fuel composition
The internal integrated flight control computer and three redundancy micro integrated navigation system (GPS/MINS) can realize one key automatic take-off, landing, hovering, circling, return, fixed altitude, parachute opening and various forms of autonomous cruise according to the scheduled route. It also provides comprehensive flight status monitoring and alarm function and perfect emergency protection mechanism to ensure the safe operation of the system.
Autonomous take-off and landing and route planning
Automatic flight beyond visual range
Control the attitude of the aircraft
Intelligent control software makes operation more convenient
Intelligent control software makes operation more convenient
Instead of manual completion of fault monitoring, emergency inspections, power planning, etc.
Pipeline leakage investigation, construction monitoring, emergency command, etc.
Nuclear emergency monitoring
Quickly realize the acquisition of geographic information
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