Product overview
The Yifei Zhineng Hercules M4-50 is a payload-carrying UAV with four rotors arranged in a four-axis configuration. Its physical architecture combines a 1700mm wheelbase with 42-inch propellers and an aviation-grade carbon-fiber airframe. The aircraft weighs 18kg unloaded and has a recommended payload of 30kg. Its maximum takeoff weight is 60kg, providing a separate total aircraft weight limit alongside the recommended payload figure.
The Hercules M4-50 cruises at 7m/s and has a maximum flight speed of 10m/s. Maximum ascent speed is 3m/s, while maximum descent speed is 2m/s. Its maximum flight radius is 15km, and its altitude ceiling is 5000m above sea level. Environmental specifications include wind resistance of 14m/s, identified as force 7, and an IP54 protection rating. The operating temperature range extends from -20°C to 50°C.
Specifications
| Specification | Value & conditions |
|---|---|
| Aircraft configuration | Four-axis quadrotor |
| Wheelbase | 1700mm |
| Airframe material | Aviation-grade carbon fiber |
| Propeller size | 42 inches |
| Empty weight | 18kgUnloaded. |
| Recommended payload | 30kg |
| Maximum takeoff weight | 60kg |
| Cruise speed | 7m/s |
| Maximum flight speed | 10m/s |
| Maximum ascent speed | 3m/s |
| Maximum descent speed | 2m/s |
| Maximum flight radius | 15km |
| Altitude ceiling | 5000m above sea level |
| Wind resistance | 14m/s (force 7) |
| Ingress protection rating | IP54 |
| Operating temperature | -20°C to 50°C |
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