S-V50 Medium Vertical Fixed Wing Unmanned Aerial Vehicle
â–² The aircraft adopts a dual strut layout with inverted V-shaped
tail wings. The tail strut is designed with an takeoff and landing
rotor system installed, with a simple and reliable structure;
â–² The rotor power adopts a 100V high-voltage motor, which has a
smaller current and higher power to weight ratio;
â–² The main power is an oil powered internal combustion engine, which has sufficient power, stable and reliable operation, and is convenient to use. The fuel is 92 # gasoline, which is easy to obtain. The aircraft can also be equipped with a multi fuel engine, which can be used with diesel, aviation kerosene, and gasoline;
â–² The body material is a carbon fiber honeycomb structure, and carbon fiber or Kevlar materials can be specially customized according to usage requirements;
â–² The front cabin designed specifically for large equipment has a larger capacity and higher load capacity.
| Item | Parameters | Item | Parameters |
| Full length | 2437mm | Maximum takeoff weight | 58kg |
| Wingspan | 4210mm | Takeoff and landing mode | Vertical takeoff and landing |
| Height | 1066mm | Cruise speed | 90-130km/h |
| Maximum task load | 10kg | Maximum battery life | 11h(Heavy oil engines) |
| Max climb rate | 5m/s | Flight mode | Manual flight, automatic route flight |
| Maximum working height | 5000m above sea level | Fuel tank capacity | 18L |
| Maximum wind resistance | Level 7 | Typical task loads | Nikon D800, Canon 5D or Photosphere, misar, 5-mount camera (optional) |
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