Description
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MH48 VTOL Large load, gasoline power fixed-wing drone Overview
The MH48 is a vertical take-off and landing (VTOL) fixed-wing UAV with hybrid power. It adopts a composite aerodynamic layout of quad-rotors and fixed wings, combining the advantages of VTOL from quad-rotor models and the long range of fixed-wing models.
Versatile Hybrid-Powered UAV for Long-Endurance Missions
Flexible and capable of adapting to various complex take-off and landing conditions, it features hybrid power with fuel and battery, achieving a long endurance, making it widely used in inspection, emergency communication, and other fields.
Overview Table of the MH48 Specifications
| Weights | |
| Maximum Take-off Weight | 64kg |
| Max. payload weight | 15kg (34kg without oil and electricity) |
| Structural weight | approximately 18Kg (including all structural and mounting parts) |
| Dimensions | |
| Dimensions | Fuselage Length: 2735mm |
| Wingspan: 4800mm | |
| Performance | |
| Endurance | 9H (540min) @ 0.5 kg load (measured near sea level at static wind) |
| Max. Cruising Speed | 201km/h (56m/s) |
| Max. Flight Altitude | 4800m |
| Maximumย windย resistance | Category 4 wind (Category 6 gusts) |
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Specifications
Specifications
Parameters for MH48
| Body material | carbon fiber, glass fiber, kevlar, PVC, etc. |
| Placement of the landing gear | below the rotor pole |
| Structural weight | approximately 18Kg (including all structural and mounting parts) |
| Maximum take-off weight | 64 kg |
| Maximum payload | 34KG (without oil and electricity) |
| Wing area | approximately 200 square metres |
| Wing load | approximately 320 g / dm2 @ 64 kg |
| Endurance | 9 H (540min) @ 0.5 kg load (measured near sea level at static wind) |
| Maximum control distance | manual remote control / about 0.5km-1km, ground station / 5km-30km |
| Standard cruising speed | 37 m / s @ 60 kg (recommended operating speed 38 m / s for mountain operations) |
| Maximum cruise speed | 201 km / h (56m / s) |
| Standard battery configuration | 48 V * 2.2Ah * 2 (45.6V) |
| Never exceed speed | 252 km / h (about 70 m / s) |
| Stall speed | 30 m / s @ 60KG (32 m / s @ roll 25 ยฐ / pitch 15 ยฐ) |
| Minimum circling radius | 300 m @ 36m / s roll 27 ยฐ (safe turning radius of not less than 350 m on plateau) |
| Maximum horizontal ascent | 4800 m above sea level |
| Wind resistance in the fixed-wing model | no less than a Category 6 wind (Category 7 gusts) |
| Maximum wind resistance in the rotor takeoff and landing mode | not less than a Category 4 wind (Category 6 gusts) |
| Drone use environment | -20 ยฐ C – 45 ยฐ C;Can fly in light rain (safe running time greater than 10min) |
| How to take off and land | vertical takeoff and landfall |
| Vertical power propeller blade size | 32 inches (recommended) |
| Fixed wing tail propulsion blades | 26 to 28 inches (recommended) |
| Maximum thrust-to-weight ratio for fixed wing | 0.55 (standard configuration) |
| Standard no-load take-off weight | approximately 42 kg |
| Safety voltage when entering the landing route | not less than 48 V (Grignard high voltage battery) |
| Wing mount angle | 2 ยฐ |
| Number of empty speed pipe installations | 2 (standardized as single empty speed tube openings) |
| Does the system support the constant power replacement of the power battery pack | Yes (not standard) |
| Fuel Consumption | 4300 RPM 2.3L / H |
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Product contents
Product contents
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| MTOW |
64kg |
|---|---|
| Cruise Speed |
37m/s |
| Max. Payload |
15kg |
| Wingspan |
4800mm |
| VTOL Type |
Hybrid |
| Frame Type |
VTOL |
| Flight Time |
9h |
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