·Large payload: max takeoff weight 100kg; endurance 4.4h with 30kg payload.
·Integrateddesign：twoinonedesignof verticaltailandandinggears,provides simple stricturept
mized aerodynamic and high power efficiency.
·Light weight and high strength:aviation carbon fiber compositematerial;circular bearing structure of
the wings,fuselage and prepreg motor arms,strengthen theflexural performance.
·Dual control surface security design:2 pcs control surfaces in the front and 4pcs in the rear,provide
dual security backup to realize opposite cooperative control.

Technical Parameter	Details
Length	2905 mm
Height	930 mm
Wingspan	Rear wing 5100 mm & Front wing 3533 mm
Airframe material	Aviation carbon fiber composites
Engine	Gasoline engine (piston engine)
Load (including fuel)	45 kg Payload & fuel
Maximum Safe Take-off Mass	100 kg
Safe Level Flight Speed	28~40 m/s
Cruising Speed	30 m/s
Comprehensive Fuel Consumption	3 L/h
Practical Ceiling	5000 m
Operating Temperature	-20℃~55℃
Wind Resistance Level	Take-off: Level 5 (8.0-10.7m/s) / Cruising: Level 6 (10.8-13.8m/s)

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