Product overview
The MUGINUAV Mugin GV600 Flight Platform carries larger sensors, communication equipment and mission systems on extended-distance missions. Its propulsion combines gasoline-powered cruise with electric vertical take-off and landing, allowing operation without a runway. Built around the Mugin GV600 Airframe Kit, the platform uses a carbon fiber composite primary structure and longer outer wing panels to achieve a 6000 mm wingspan. Overall dimensions are approximately 6000 × 3500 × 960 mm, with a wing area of 312 dm².
The physical layout includes two-piece VTOL booms for easier packing, transport and handling, reinforced boom structures and inner ribs, and integrated motor mounting points with a 5° offset. The equipment cabin accommodates payloads, avionics, communications hardware and other onboard systems. Reference fuselage internal dimensions are approximately 1800 × 368 × 393 mm; usable installation space depends on the equipment fitted. The supplied flight platform has its propulsion, flight control, power system and actuators installed and configured, while mission payloads, data links and ground control equipment can be selected for the application.
Maximum take-off weight is 110 kg and maximum payload is 25 kg. The reference configuration has a 30 L fuel tank, but payload and fuel combinations change endurance: approximately 1.8 hours with 25 kg and 12 L, 3.9 hours with 20 kg and 23 L, or 5 hours with 15 kg and 30 L. Maximum payload and maximum endurance therefore represent different operating conditions. Reference range exceeds 500 km; endurance and range vary with payload, fuel load, flight conditions, altitude, weather and mission profile.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | MUGINUAV Mugin GV600 Flight Platform |
| Intended payload applications | Transport of larger sensors, communication equipment and mission systems over extended distances. |
| Overall dimensions | Approx. 6000 × 3500 × 960 mmReference dimensions. |
| Fuselage internal dimensions | Approx. 1800 × 368 × 393 mmReference dimensions; usable installation space depends on fitted systems and equipment. |
| Wing area | 312 dm² |
| Primary structure | Carbon fiber composite |
| Propulsion | Gasoline cruise + electric VTOL |
| Fuel tank capacity | 30 LReference Flight Platform configuration. |
| Maximum take-off weight | 110 kg |
| Maximum payload | 25 kgMaximum payload and maximum endurance apply to different operating conditions. |
| Maximum speed | 40 m/s |
| Cruise speed | 30-35 m/s |
| Stall speed | 25 m/s |
| Endurance | Up to 5 hours (reference)Reference endurance with a 15 kg payload and 30 L of fuel; varies with payload, fuel load, flight conditions, altitude, weather and mission profile. |
| Flight range | Greater than 500 kmReference range; depends on payload, fuel load, flight profile and operating conditions. |
| Wind resistance | VTOL Level 4 / Fixed-wing Level 6VTOL and fixed-wing flight modes respectively. |
| Reference endurance at 25 kg payload | Approx. 1.8 hours25 kg payload; 12 L fuel load. |
| Reference endurance at 20 kg payload | Approx. 3.9 hours20 kg payload; 23 L fuel load. |
| Reference endurance at 15 kg payload | Approx. 5 hours15 kg payload; 30 L fuel load. |
| Airframe and wing architecture | Built around the Mugin GV600 Airframe Kit, with longer outer wing panels providing a 6000 mm wingspan. |
| VTOL boom construction | Two-piece VTOL booms with reinforced structure and inner ribs; designed for easier packing, transportation and handling. |
| VTOL motor mounting | Integrated VTOL motor mounting points with a 5° offset angle. |
| Equipment cabin | Large cabin accommodating payloads, avionics, communication equipment and other onboard systems.Usable installation space depends on fitted systems and equipment. |
| Installed equipment | Complete flight platform with propulsion, flight control, power system and actuators installed and configured.Complete Flight Platform configuration. |
| Project-specific equipment | Application-specific selection of mission payloads, data links, ground control equipment and other project systems.Selected according to the application. |
| Runway requirement | Supports operation without a runway.Electric vertical take-off and landing. |
| Endurance limitations | Maximum payload and maximum endurance are achieved under different operating conditions.Reference payload, fuel load and endurance combinations. |
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