Product overview
The Guangdong Fanya Technology EM-D150 is a four-axis, eight-propeller transport UAV for supplying special military and police operations. Its high-strength titanium-alloy main structure has a detachable airframe and landing gear, while propulsion uses T-MOTOR motors and propellers. The protective case has a split design. The aircraft configuration includes triple-redundant flight control, a standard whole-aircraft parachute with inadvertent-activation protection, and an HD digital image-transmission system for live video monitoring. Loss-of-control return and broken-propeller protection are additional flight-control functions.
Integration capabilities include UAV management-platform connectivity, command-system interfacing and ADS-B. The ground station supports route planning, autonomous or semi-autonomous flight, and live battery, flight-data and position displays. General load ratings are 150 kg maximum and 130 kg rated, while mission configurations specify 100 kg for routine sea-level operations, 200 kg at sea level with a custom battery, or 100 kg at 3000 m with a custom battery. Sea-level endurance exceeds 30 minutes unloaded and 15 minutes carrying 100 kg. Control distance is 15 km in open, unobstructed conditions.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | Guangdong Fanya Technology EM-D150 |
| Aircraft architecture | Four-axis, eight-propeller multirotor with a high-strength titanium-alloy main structure; detachable airframe and landing gear. |
| Protective case | Split-design protective case. |
| Propulsion components | T-MOTOR motors and propellers. |
| General load ratings | Maximum load: 150 kg; rated load: 130 kg. |
| Wheelbase | 2635 mm |
| Wind resistance | Maximum wind resistance: Force 6. |
| Flight range | 15 km |
| Control distance | 15 kmOpen, unobstructed conditions. |
| Maximum takeoff weight | 330 kgAt sea level. |
| Onboard GPS module interface | DroneCAN communication protocol, 8 Mbit/s. |
| Navigation receiver and satellite systems | High-precision, multi-frequency GNSS receiver; GPS, GLONASS, Galileo and BeiDou + SBAS and QZSS. |
| Satellite frequency bands | B1I, B2a, E1B/C, E5a, L1C/A, L1OF, L5 |
| Position accuracy | 0.01 m + 1 ppm CEP |
| Mission payload configurations | Sea level: 200 kg with a custom battery, or 100 kg for routine operations; 3000 m altitude: 100 kg with a custom battery.200 kg at sea level requires a custom battery; 100 kg at sea level is for routine operations; 100 kg at 3000 m altitude requires a custom battery. |
| Cruise speed | 5–10 m/s |
| Maximum flight speed | 30 km/h |
| Maximum flight height | 500 m |
| Operating temperature | −10°C to 50°C |
| Mission response time | Less than 51 min |
| Intended mission | Supply transport in special military and police scenarios. |
| Remote-control distance | 15 kmOpen, unobstructed conditions; ordinary signal. |
| Flight endurance | Unloaded: greater than 30 minutes; carrying 100 kg: greater than 15 minutes.At sea level, unloaded or carrying 100 kg as specified. |
| Flight-control redundancy and protection | Triple-redundant flight control, loss-of-control return and broken-propeller protection. |
| Ground-station functions | Real-time battery-level and flight-parameter display. |
| Mission control and integration | Route planning; autonomous and semi-autonomous flight; real-time flight-data and latitude/longitude display; equipped HD digital image transmission for live video monitoring; command-system integration. |
| UAV management-platform connectivity | Interconnection with a UAV management platform. |
| Separate-site operation and return | Takeoff and landing at different sites; one-button return using a physical aircraft button without a remote controller after arrival at point B.After flying from point A to point B. |
| Parachute equipment and protection | Standard whole-aircraft parachute with protection against inadvertent activation.Whole-aircraft parachute supplied as standard. |
| ADS-B | ADS-B functionality. |
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