Product overview
Guangdong Fanya Technology’s EM-003 is a fuel-electric hybrid flight platform for emergency rescue, aerial reconnaissance, medical applications, military and police operations, maritime anti-smuggling, forestry and forest-fire patrols. Its X-shaped structure has a symmetrical wheelbase of ≤1300 mm. An integrated fuel tank uses anti-slosh baffles and antistatic protection, while the fuel system incorporates a backup circuit. The aircraft provides whole-aircraft rain and water protection and touchscreen remote starting. A whole-aircraft parachute and the ability to take off and land at different locations are standard.
Engine power is ≤2.5 kW, with a maximum takeoff weight of 19 kg at sea level. Flight time exceeds three hours with ≤4 L of fuel; immediate takeoff after landing and refuelling supports operation exceeding 12 hours per day. Range is 80 km, cruising speed is 18 m/s, and maximum speed is specified as 22 m/s and separately as 80 km/h. Operating limits include Level 7 wind resistance, a maximum flight height of 2000 m and temperatures from -20°C to 50°C. The 15 km control radius requires open, unobstructed surroundings; unlimited-distance remote control requires a 5G signal.
Integration features include a ground station, HD digital image transmission, command-system connectivity and cloud management. The ground station supports route planning, autonomous or semi-autonomous flight and live fuel-consumption, engine-power and coordinate displays. Cloud functions cover fleet dispatch, flight-data analysis, remote flight commands and payload-pod controls such as zoom, recording and false-colour selection. Platform video and data return have latency below 300 ms. The parachute deploys automatically during flight at battery voltage below 40 V, tilt above 45° or gravity-assisted downward speed above 10 m/s. Autonomous flight supports the four specified communication-loss scenarios.
Specifications
| Specification | Value & conditions |
|---|---|
| Aircraft architecture and protection | Fuel-electric hybrid UAV with an X-shaped structure, all-weather flight capability, whole-aircraft rain and water protection, remote starting and a standard whole-aircraft parachute.Whole-aircraft parachute supplied as standard. |
| Symmetrical wheelbase | ≤1300 mm |
| Wind resistance | Level 7 |
| Range | 80 km |
| Engine power | ≤2.5 kW |
| Maximum takeoff weight | 19 kgAt sea level. |
| Fuel supply and monitoring | Dual-path fuel collector, backup fuel circuit and real-time fuel-consumption display at the ground station. |
| Cruising and maximum speeds | Cruising speed: 18 m/s; maximum speed: 22 m/s; maximum flight speed also specified as 80 km/h. |
| Maximum flight height | 2000 m |
| Operating temperature | -20°C to 50°C |
| Fuel tank construction | Integrated fuel tank with antistatic protection and anti-slosh baffles to reduce fuel movement during high-speed flight. |
| Mission applications | Emergency rescue, aerial reconnaissance, medical applications, military and police operations, maritime anti-smuggling, forestry and forest-fire patrols. |
| Remote-control reach | Operating radius: 15 km; 5G-based remote operation specified as having unlimited distance.15 km operating radius in open, unobstructed surroundings; unlimited-distance remote operation requires a 5G signal. |
| Endurance and refuelling | Flight time greater than 3 hours; immediate takeoff after landing and refuelling; sustained operation greater than 12 hours/day.With ≤4 L of fuel; repeated operation includes landing and refuelling. |
| Automatic parachute deployment thresholds | Automatic deployment at monitored battery voltage less than 40 V, aircraft tilt greater than 45°, or gravity-assisted downward speed greater than 10 m/s.During flight. |
| Ground station and command-system integration | Route planning, autonomous and semi-autonomous flight, real-time engine-power and latitude/longitude displays, HD digital image transmission and command-system connectivity.HD digital image-transmission system included. |
| Cloud flight-data transmission and analysis | Real-time flight-data return, per-aircraft data aggregation, analysis and visualisation, including an attitude indicator.Flight-data return through QGC ground-station transmission or a cloud app. |
| Fleet management and remote coordination | One-controller management of multiple aircraft, mission assignment, central tracking, control and dispatch, with interaction between remote managers and field operators. |
| Video return latency and display | Latency less than 300 ms; multiple live-video windows with basic flight-data display.For in-flight video and data returned through the platform. |
| Remote flight controls | Takeoff, landing, return, position-hold and guided modes, parachute activation, and virtual-joystick control of ascent, descent, yaw, forward/backward and lateral movement.Through the management platform. |
| Payload-pod integration functions | Pod pitch, yaw, zoom, photography, recording, one-touch centring, downward pointing, false-colour switching, camera-core restart and video restart.Through the platform's remote payload-pod controls. |
| Remote dispatch communications | Video and voice links between the command centre, field operators and operational command vehicles. |
| Access management | Hierarchical management with permission-based account allocation and equipment and personnel control. |
| QR-code sharing and video conferencing | QR-code sharing of live flight data, payload-pod video, coordinates and flight tracks; video conferencing from the shared page with aircraft-specific or custom meeting numbers. |
| Engine service life | ≥300 hours |
| Starting method | Touchscreen remote starting. |
| Different-site takeoff and landing | Takeoff and landing at different locations.Standard configuration. |
| Autonomous flight during link loss | Autonomous flight capability under four communication-loss scenarios.Network, remote-control signal, image-transmission and data-transmission loss scenarios. |
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