Product overview
The Mugin GF360 Airframe Kit is a Mugin 3 series fixed-wing airframe intended for teams installing their own propulsion, flight systems and mission equipment. Its twin-boom architecture combines an H-tail with a rear gasoline pusher installation, preserving the central fuselage for onboard systems and payload hardware. The kit supplies fuselage, wing and H-tail assemblies, tail booms, wheeled landing gear and installation accessories. Propulsion, servos, flight control, electrical systems, communications and ground control require project-specific selection and integration; the final supply scope is defined by the quotation.
The structure is primarily carbon fiber composite, manufactured using hot-press molding in high-precision steel molds. Fiberglass front fuselage and center-wing hatches provide installation locations for internal antennas and radio equipment. Both openings give access to equipment areas, while the center-wing opening permits refueling with the wing installed and can accommodate a parachute compartment. Overall reference dimensions are approximately 3500 × 2521 × 870 mm, with approximately 1255 × 262 × 293 mm inside the fuselage; usable installation space depends on equipment layout.
Wheeled landing gear supports runway operations; catapult or assisted takeoff requires suitable modifications and project-specific launch equipment. Airframe weight is approximately 13.5 kg excluding propulsion and flight systems. The recommended take-off weight is 27–33 kg, distinct from the 45 kg structural limit. Payload capacity depends on the completed configuration, and operating weight and flight performance depend on installed systems and fuel load. Recommended cruise airspeed is 24–26 m/s; the 19 m/s stall speed applies to a configured reference aircraft at 30 kg MTOW.
Specifications
| Specification | Value & conditions |
|---|---|
| Product identity | Mugin GF360 Airframe Kit, Mugin 3 series |
| Supplied product type | Airframe kit requiring integration of propulsion, flight systems and mission equipment |
| Airframe layout | Twin-boom layout with rear gasoline pusher installation and central fuselage space for flight systems and mission hardware |
| Dimensions | Approx. 3500 × 2521 × 870 mmDimensions are reference values. |
| Fuselage internal dimensions | Approx. 1255 × 262 × 293 mmDimensions are reference values. Usable internal space depends on the equipment layout. |
| Wing area | 1.33 m² |
| Primary structure | Carbon fiber composite with fiberglass hatches |
| Propulsion design | Designed for gasoline pusher propulsion |
| Fuel tank capacity | 14 L / 10 L (Optional)10 L option. |
| Maximum structural weight limit | 45 kgThe structural weight limit is not the recommended take-off weight. |
| Maximum payload | Depends on final configurationDepends on installed systems and fuel load. |
| Recommended maximum speed | 35 m/sAirspeed. |
| Recommended cruise speed | 24–26 m/sAirspeed. |
| Stall speed | 19 m/sAirspeed at 30 kg MTOW on a configured GF360 reference aircraft. |
| Wind resistance | VTOL N/A / Fixed-wing Level 6VTOL: N/A; fixed-wing operation. |
| Airframe weight | Approx. 13.5 kgExcludes propulsion and flight systems. |
| Recommended take-off weight | 27–33 kg |
| Recommended pusher propeller | 21–25 inches |
| Recommended VTOL propeller | N/A |
| Manufacturing process | Hot-press molding in high-precision steel molds |
| Equipment access | Front and center-wing access hatches; center-wing opening supports refueling with the wing installed and can accommodate a parachute compartment |
| Internal antenna installation locations | Fiberglass front fuselage and center-wing hatches provide locations for internal antennas and radio equipment |
| Kit contents | Fuselage, wing and H-tail assemblies, tail booms, wheeled landing gear and installation accessoriesFinal supply scope is defined by the quotation. |
| Systems to integrate | Propulsion system, servos, flight controller, electrical equipment, communication links and ground control equipmentProject integration around the mission payload. |
| Takeoff arrangements | Wheeled runway operations; catapult or assisted takeoff requires suitable airframe modifications and launch equipmentCatapult or assisted takeoff requires project-specific modifications and launch equipment. |
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