Product overview
The MMC UAV M11 is a payload-carrying fixed-wing flight platform with vertical takeoff and landing. Its carbon-fiber and glass-fiber airframe has a 4800 mm wingspan, a length of 2580 mm and a height of 850 mm. Maximum takeoff weight is 55 kg, and maximum payload weight is 15 kg. Transport packaging comprises a 181 × 98 × 72 cm aircraft case and a 180 × 46 × 111 cm wing case. Assembly and deployment take two people less than three minutes, with a 3 × 3 m area specified for takeoff and landing.
The eight-battery configuration uses eight 30000 mAh 6S batteries and has an endurance of 180 minutes and a range of 200 km. The ten-battery configuration uses ten batteries of the same specification, with 220 minutes of endurance and 240 km of range. Cruise speed is 27 m/s, approximately 97 km/h; maximum flight speed is 40 m/s, approximately 144 km/h. The control radius is 80 km. Fully autonomous takeoff and landing, dual-redundant communications, return on signal loss or low voltage, overturn rotor protection and emergency remote control support flight operations.
Operating limits include a maximum altitude ceiling of 4500 m above sea level and an ambient temperature range of -20 to 60 °C. Maximum wind resistance is Force 7, while IP54 protection covers light rain. At sea level, the climb and descent speed is ±3 m/s. Hovering accuracy is ±1 m vertically and ±1 m horizontally. These environmental and flight limits accompany the two battery configurations; their respective endurance and range figures remain distinct from the aircraft's 80 km control radius.
Specifications
| Specification | Value & conditions |
|---|---|
| Aircraft type | Vertical-takeoff-and-landing fixed-wing UAV. |
| Aircraft dimensions |
|
| Packaging dimensions | Aircraft case: 181 × 98 × 72 cm; wing case: 180 × 46 × 111 cm. |
| Airframe materials | Carbon fiber and glass fiber. |
| Climb and descent speed | ±3 m/s.At sea level. |
| Cruise speed | 27 m/s, approximately 97 km/h. |
| Battery configuration | 8 × 30000 mAh 6S batteries.Eight-battery version. |
| Battery configuration | 10 × 30000 mAh 6S batteries.Ten-battery version. |
| Maximum altitude ceiling | 4500 m above sea level. |
| Operating ambient temperature | -20 to 60 °C. |
| Position accuracy | Vertical: ±1 m; horizontal: ±1 m.During hovering. |
| Endurance | 180 min.Eight-battery version. |
| Endurance | 220 min.Ten-battery version. |
| Assembly and deployment time | Less than 3 minutes.Two-person assembly and deployment. |
| Maximum takeoff weight | 55 kg. |
| Maximum payload weight | 15 kg. |
| Maximum flight speed | 40 m/s, approximately 144 km/h. |
| Control radius | 80 km. |
| Communications data link | Dual-redundant 1.4 GHz and 450 MHz data links. |
| Maximum wind resistance | Force 7. |
| Ingress protection | IP54; protection against light rain. |
| Takeoff and landing area | 3 × 3 m. |
| Flight range | 200 km.Eight-battery version. |
| Flight range | 240 km.Ten-battery version. |
| Takeoff and landing mode | Fully autonomous takeoff and landing. |
| Safety functions | Return on communications loss or low voltage; rotor protection if overturned; emergency remote control. |