1. General Specifications & Dimensions

• Configuration: Main rotor plus tail rotor (tail rotor directly driven by motor)
• Fuselage Dimensions (excluding main rotor): 3400 × 960 × 1200 mm (Length × Width × Height)
• Main Rotor Diameter: 3635 mm
• Tail Rotor Diameter: 815 mm
• Maximum Takeoff Weight (MTOW): 160 kg
• Empty Weight: Approx. 85 kg (calculated by subtracting maximum payload from MTOW)

2. Power System & Fuel

• Engine: 210 cc horizontally opposed twin-cylinder liquid-cooled piston engine (independently developed)
• Power Output: Approx. 28 kW / 38 HP
• Fuel Type: 92# gasoline / aviation kerosene
• Fuel Tank: Built-in 10 L + external 30 L, total 40 L
• Power Supply: Integrated generator + backup battery

3. Flight Performance

• Maximum Level Flight Speed: 126 km/h
• Cruising Speed: 90–110 km/h
• Service Ceiling: 3000 m
• Wind Resistance: Stable operation under Level 6 wind (approx. 13.8 m/s)
• Operating Temperature: −20 ℃ ~ +50 ℃
• Hover Accuracy (GPS): Horizontal ±2 m, Vertical ±1 m

4. Payload & Endurance

• Maximum Payload: 75 kg (including fuel)
• Typical Mission Payload: 55 kg

Flight Endurance

• No load: 250 minutes (approx. 4 hours 10 minutes)
• 55 kg payload: 120 minutes (2 hours)
• Control Range: 25 km (line of sight); Relay-supported beyond visual range operation available
• Video Transmission Range: 25 km (high-definition)

5. Flight Control & Mission Equipment

• Flight Control System: Self-developed flight controller, supporting fully autonomous takeoff, landing and route flight
• Standard Optional Payload: 2-axis triple-sensor gimbal pod
  • Visible Light Camera: 30× optical zoom
  • Thermal Imaging Camera: 640×512 resolution
  • Laser Rangefinder: Maximum range 3 km
• Expandability: Compatible with custom third-party payloads for mapping, inspection, airdrop and other missions

6. Application Scenarios