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HC-332E long-endurance electric unmanned aerial vehicle

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1. Airframe & Structure

  • Configuration: Hexacopter, Vertical Takeoff and Landing (VTOL)
  • Diagonal Wheelbase: 1560 mm
  • Dimensions (Unfolded): 1560 × 1560 × 480 mm
  • Empty Weight: 7.8 kg (excluding battery and payload)
  • Maximum Takeoff Weight (MTOW): 19 kg
  • Payload: Standard 2 kg / Maximum 5 kg
  • Airframe Material: Full carbon fiber composite material
  • Arms: Detachable with quick-release design
  • Ingress Protection: IP54 (dustproof & light rain resistant)
  • Transport Case Dimensions: 980 × 720 × 600 mm

2. Flight Performance

Powered by semi-solid lithium battery
  • Endurance:
    • 60 mins @ 2 kg payload (Nominal)
    • 50 mins @ 2 kg payload (Typical actual)
    • 40 mins @ 5 kg full load
  • Cruising Speed: 0–12 m/s (0–43.2 km/h)
  • Maximum Level Flight Speed: 15 m/s (54 km/h)
  • Service Ceiling: 3000 m above sea level
  • Wind Resistance: Stable cruising under Level 6 wind (12–13.8 m/s)
  • Operating Temperature: −20 ℃ ~ +50 ℃
Hover Accuracy (GPS + BeiDou):
  • Horizontal: ±0.5 m
  • Vertical: ±0.5 m
  • Attitude Stability Accuracy: ±1°

3. Power System

  • Battery Model: IB‑25H Semi-solid Smart Lithium Battery
  • Capacity: 25 Ah
  • Voltage: 44.4 V (12S)
  • Single Battery Weight: Approx. 4.2 kg
  • Energy Density: 30–35% higher than traditional lithium polymer batteries
  • Motor: TMU8II Brushless Motor, 85 KV
  • ESC: 60 A Brushless Electronic Speed Controller
  • Propeller: 29 × 9.5 inch (Quick-release type)

4. Flight Controller & Navigation

  • Flight Control System: HC‑Flight Multi-rotor Flight Controller (Dual redundancy)
  • Navigation System: Dual GPS + Dual IMU + BeiDou + Barometer + Magnetometer
  • Flight Modes: Manual mode, Attitude mode, GPS Hover, Waypoint Navigation, Autonomous Takeoff & Landing, Beyond Visual Line of Sight (BVLOS)
  • Control Range (Data Radio): Optional 10 km / 20 km / 30 km
  • 5G Version: Supports 5G video transmission and remote control (unlimited range within network coverage)
Safety Features: Multiple no-fly zones, Low battery return-to-home, Loss-of-control protection, One-key return-to-home, Parachute protection (optional)

5. Compatible Payloads

  • EO Pod: Single-light (40× zoom / AI recognition), Dual-light (Thermal + Visible Light), Triple-light (Thermal + Visible Light + Laser Rangefinder)
  • Mapping Camera: Orthographic camera, 5-lens oblique aerial camera
  • LiDAR: 16-line / 32-line, applicable for power line inspection, forestry and topographic mapping
  • Others: Gas detector, Loudspeaker, Aerial nuclear spectrometer, Custom third-party payloads

6. System Composition

  • Flight platform (Hexacopter airframe + Motors + ESCs + Propellers)
  • Standard equipped with 1 × semi-solid lithium battery
  • Flight controller + Dual GPS/IMU navigation module
  • Data radio (10/20/30 km optional)
  • Ground Control Station (GCS‑D01, handheld / tablet type)
  • Mission payload (optional)
  • Transport case, tool kit and spare propellers

7. Reliability & Service Life

  • Mean Time Between Failures (MTBF): 500 hours
  • Design Service Life: ≥ 5 years under regular maintenance
  • Operating Environment: Stable operation in light rain, Level 6 wind and temperature down to −20 ℃
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