The cruise engine and propeller are positioned in front of and behind the mid-section of the aircraft, maintaining a streamlined fuselage while enhancing propulsion efficiency, ensuring clean airflow over the main wing and reducing overall drag. The engine's upper position frees up space and payload capacity, allowing it to carry more payload. The payload bay is also easily adjustable.
The aircraft features dual redundant backup, ensuring safe return to base even in the unlikely event of a malfunction of a control surface or power unit.
To meet diverse customer needs, we offer a trolley version of the fixed-wing UAV. Compared to the VTOL version, it is lighter, offers a greater payload capacity, and offers longer flight time.
Technical Specifications
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Length
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3930 mm
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Height
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1775.5 mm
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wingspan
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8000mm
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Airtrame materia
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Awiationcabon fiber composines
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Engine
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Gasoline engire
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Load
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vT0L75 kg|Taxing130 kg
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Take-orf mass
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vT0L170 kg|Taxding180 kg
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Levelspeed
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26-45 m/s
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cruising speed
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28 m/s
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Fuelcoms
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vT0L7.5 L/h|Taxing 7L/h
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Max range
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vT0L400KM|Texiing 428km
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Auitude
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5000 m
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Temperature
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-20°C-45°C
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wind resistance
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take-ofleve.5/cruisinglevel6
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Protectian degree
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IPX4
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