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Current Location:Home > Product Center > HC-332H Hybrid power UAV
HC-332H Hybrid power UAV

Extra long endurance creates more possibilities

★ The products are subject to the real products sold in the market ★
Advantages and features

Through systematic design innovation, the flight performance, use experience and reliability have been greatly improved. The fuselage is airtight, which can operate in light rain, quickly disassemble the structure and facilitate transportation; Universal platform, which can quickly replace various task loads.

  • Max payload 5kg

  • Max endurance 210min

  • Hybrid power system

  • Accumulated flight 500h without failure

  • Multi-GPS redundant design

  • Autonomous flight beyond visual range

  • Compatible with multiple load platforms

GX-2 Hybrid power system
Strong power

After long-term testing, optimization and in-depth adjustment
the GX-2 hybrid power system has the advantages of stable output power and high reliability, effectively improving the operation time and operation radius.

One UAV for multiple purposes
and the flight platform is compatible with multiple loads
Carrying different payloads to achieve UAV multi-purpose
HC-332H
How far can the oil-electric power system fly

HC-332H Equipped with 5L super large fuel tank, H2 engine has high fuel utilization. 1L fuel can fly 54km, and the flight time is up to 1 hour.

  • 5L

    Tank capacity

  • 210min

    Estimated flight time

  • 150km

    Estimated flight distance

  • Ratio of gasoline & engine oil 25:1

    Fuel composition

Intelligent flight control system

The flight control system has the ability of multi-rotor hovering, autonomous take-off and landing and route planning, and supports the automatic flight beyond visual range. Support switching flight mode online (auto/manual); It can control the flight state of the aircraft such as attitude, altitude, heading and position to achieve stable and reliable automatic flight. Dual control mode can adjust the flight plan at any time (based on the way point); External data transmission station; Dual GPS and dual IMU are adopted to realize system redundancy and backup. With multiple functional restrictions in no-fly zone.

  • Autonomous Takeoff And Landing And Route Planning

  • Over The Horizon Automatic Flight

  • Control The Attitude Of The Aircraft

  • Online Switching Flight Mode

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