S-150 Medium Vertical Takeoff and Landing Unmanned Aerial Vehicle System
The S-150 drone adopts a dual tail strut layout, a high lift to drag ratio airfoil, and an inverted V-shaped tail. The tail strut is
designed with an takeoff and landing rotor system installed, with a simple and reliable structure;
â–²The S-150 drone adopts a dual tail strut layout, a high lift to drag ratio airfoil, and an inverted V-shaped tail. The tail strut is
designed with an takeoff and landing rotor system installed, with a simple and reliable structure;
â–² The aircraft has a large wing area and a large payload, with a maximum load of up to 30kg;
â–² The rotor system adopts a four axis 8-rotor motor, which has high efficiency in asynchronous rotation up and down. When
one motor fails, the other motors can still safely land the aircraft, making dual redundancy power safer;
â–² The power adopts a 100V specially designed high-performance high-voltage motor, with smaller current and stronger power;
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
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