Product overview
The Yifei Zhineng Hercules M6-X13 is a six-rotor UAV intended to carry heavy equipment, with a maximum payload of 80kg and reserved mounting space beneath the aircraft. Its structure uses high-strength carbon fiber and aviation-grade aluminum alloy, while the airframe material specification lists aviation carbon fiber and aviation composites. The aircraft unfolds for operation within five minutes. Its 2600mm wheelbase accompanies unfolded dimensions of 3360*3360*1148mm and folded dimensions of 1001*1001*785mm, both excluding propellers. Empty aircraft weight is 75kg without batteries, and maximum takeoff weight is 160kg.
The standard configuration supplies a frame, remote controller, four 18S 40AH batteries, charging equipment, six motors, six propellers, installation tools, a custom onboard wiring harness, documentation and a custom packaging box. Maximum unloaded endurance is 70min; maximum horizontal speed is 15m/s and maximum flight radius is 15km. Operating limits include a 5000m maximum takeoff altitude, Level 6 wind resistance, IP54 protection and an ambient temperature range of -20°C to 50°C. Horizontal hovering accuracy is ±0.5m under good satellite positioning conditions. Aircraft parameters can be customized, with the delivery contract governing the agreed configuration.
Specifications
| Specification | Value & conditions |
|---|---|
| Product identity and architecture | Yifei Zhineng Hercules M6-X13 six-rotor UAV. |
| Deployment time | Can unfold for operation within 5 minutes. |
| Construction materials | High-strength carbon fiber and aviation-grade aluminum alloy; the airframe specification additionally lists aviation carbon fiber and aviation composite materials. |
| Airframe material specification | Aviation carbon fiber and aviation composite materials. |
| Payload integration space | Reserved customization space beneath the aircraft supports installation of heavy equipment and other payloads. |
| Customization basis | Aircraft parameters can be customized; the delivery contract governs the agreed configuration.Customized aircraft parameters. |
| Wheelbase | 2600mm |
| Unfolded dimensions | 3360*3360*1148mmExcluding propellers. |
| Folded dimensions | 1001*1001*785mmExcluding propellers. |
| Maximum flight endurance | 70minUnloaded aircraft. |
| Empty aircraft weight | 75kgExcluding batteries. |
| Maximum payload | 80kg |
| Maximum takeoff weight | 160kg |
| Cruising speed | No numerical value specified; unit listed as m/s. |
| Maximum horizontal flight speed | 15m/s |
| Maximum ascent speed | 5m/s |
| Maximum descent speed | 2.5m/s |
| Maximum flight radius | 15km |
| Maximum takeoff altitude | 5000m above sea level |
| Wind resistance | Level 6 |
| Ingress protection | IP54 |
| Operating ambient temperature | -20°C to 50°C |
| Maximum tilt angle | 28° |
| Horizontal hovering accuracy | ±0.5mGood satellite positioning conditions. |
| Frame and remote controller | 1 Hercules M6-X13 frame set and 1 remote controller.Standard supplied configuration. |
| Power batteries | 4 batteries, 18S 40AH.Standard supplied configuration. |
| Charging equipment | 1 charging unit.Standard supplied configuration. |
| Motors and propellers | 6 EF Motor motors and 6 EF Propeller propellers, listed as CW/CCW.Standard supplied configuration. |
| Installation tools and onboard wiring | 1 installation tool kit and 1 custom onboard connection wiring harness set.Standard supplied configuration. |
| Documentation and packaging | 1 documentation set containing a conformity certificate and instruction manual, plus 1 custom packaging box.Standard supplied configuration. |
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