technical specification
flight system
Range duration：4 – 6 hours(Non-altitude areas) Stall speed：95km/h
Cruise speed：120 to 140 kilometers per hour
Maximum flight speed： 160km/h Practical ceiling：5000m
Maximum mission payload ： 30kg Maximum takeoff weight：145kg
Landing and takeoff method：vertical take-off and landing
Body material ；carbon fibre composite Power system Fuel：Two-cylinder two-stroke piston engine
Fuel：95# or higher unleaded gasoline, 1 : 50 fully synthetic lubricating oil Fuel tank capacity：40L
