Product overview
The MUGINUAV Mugin GV293 Flight Platform supports projects needing vertical departure and landing alongside extended fixed-wing cruise. Electric motors handle vertical flight, and a gasoline engine provides cruise propulsion after transition. Its carbon fiber composite structure has a 2930 mm wingspan and a 97 dm² wing area. Maximum take-off weight is 23 kg, with a maximum payload of 3 kg and a 5 L fuel tank. This architecture enables operation without a runway.
The fuselage offers approximately 1017 × 221 × 216 mm of internal space for flight systems, communications equipment and mission payloads. Overall dimensions are approximately 2930 × 2021 × 701 mm; both dimensional measurements can vary with configuration, antennas and integrated equipment. Each boom separates into two sections for packing and transport. Reinforced boom structures and internal ribs support repeated field use, while structurally integrated VTOL motor mounting bases incorporate a 5-degree offset.
The supplied configuration is a complete flight platform with integrated propulsion, flight control, power and actuation systems. Payloads, data links, ground control and communications equipment are selected for the project. Cruise speed is 21-23 m/s, with a 30 m/s maximum and an 18 m/s stall speed. Endurance reaches up to 5 hours and range up to 300 km, but maximum figures are not simultaneous: reference endurance is 4.5 hours with 1 kg payload and 5 L fuel, or 2 hours with 3 kg and 2.5 L. Endurance varies with operating conditions and configuration; wind resistance is Level 4 in VTOL and Level 6 in fixed-wing flight.
Specifications
| Specification | Value & conditions |
|---|---|
| Product identity | MUGINUAV Mugin GV293 Flight Platform |
| Dimensions | Approx. 2930 × 2021 × 701 mmActual dimensions may vary depending on platform configuration, antenna installation and integrated equipment. |
| Fuselage Internal Dimensions | Approx. 1017 × 221 × 216 mmActual dimensions may vary depending on platform configuration, antenna installation and integrated equipment. |
| Wing Area | 97 dm² |
| Primary Structure | Carbon Fiber Composite |
| Propulsion | Gasoline Cruise + Electric VTOL |
| Fuel Tank Capacity | 5 L |
| Maximum Take-off Weight | 23 kg |
| Maximum Payload | 3 kg |
| Maximum Speed | 30 m/s |
| Cruise Speed | 21-23 m/s |
| Stall Speed | 18 m/s |
| Endurance | Up to 5 hoursEndurance varies with payload, fuel load, flight profile, environmental conditions and system configuration. |
| Flight Range | Up to 300 km |
| Wind Resistance | VTOL Level 4 / Fixed-wing Level 6VTOL and fixed-wing flight modes, respectively. |
| Wingspan | 2930 mm |
| Boom construction | Two sections per boom; reinforced boom structure and internal ribs |
| VTOL motor mounting bases | Structurally integrated with a 5-degree offset angle |
| Reference endurance with 1 kg payload | 4.5 Hours1 kg payload and 5 L fuel load; endurance varies with flight profile, environmental conditions and system configuration. |
| Reference endurance with 3 kg payload | 2 Hours3 kg payload and 2.5 L fuel load; endurance varies with flight profile, environmental conditions and system configuration. |
| Supplied configuration | Complete VTOL flight platform with integrated propulsion, flight control, power and actuation systems |
| Mission equipment selection | Project-selected payloads, data links, ground control equipment, communication equipment and other mission-specific devicesSelected according to project requirements. |
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