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AF-C100-1

AF-C100-1

WhatsAPP : +86 153 7183 2809

WhatsAPP : +86 153 1216 2872

AF-C100-1 is a type of tandem wing layout with vertical take-off and landing fixed wing UAV platform,of which the fuselage is made of aviation carbon fiber composite material.it is characterized byhigh strength and light weight, suitable for various application such as long flight time, largeload and weight tasks.
The front wing is down reversed and the rear wing is up-reversed, a perfect combination ofaerodynamics and design aesthetics, The machine adopts extremely high lift resistance ratioand large chord ratio wing design, which makes full use of wing area load capacity, minimizeunnecessary aerodynamic resistance.

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  • Length 2905 mm
    Height 930 mm
    Wing span Rear wing 5100 mm & Front wing 3530 mm
    Airframe material Aviation carbon fiber composites
    Engine Gasoline engine
    Load 45 kg
    Take-off mass 100 kg
    Level speed 28~45 m/s
    Cruising speed 30 m/s
    Fuel consumption 4L/h
    Max range 810 km

    AF-C100-1

    * All performance data in the foregoing pages are theoretical values obtained by UAVCrafts® internal laboratories through tests carried out under particular conditions.

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