Energy source: hybrid electric vehicle
Power layout: 4+1 power layout
Structure: Composite Wing Aircraft
Takeoff weight: 700KG
Cruise speed: 180km/h
Cruise altitude: 300-600 meters (up to 3000 meters)
Maximum range: 1200 kilometers
Number of seats: 2

Vertical takeoff and landing, convenient and fast: does not rely on airplane runways, intelligent flight control, simple operation.
Long endurance and large cruising radius: Vertical takeoff and landing endurance of 4.5 hours, flight distance of 800 kilometers, gliding takeoff and landing, maximum range of 1200 kilometers
Safe and reliable: 8 electric vertical takeoff and landing units, able to fly normally even with some malfunctions, and can glide and land in the event of a complete loss of power; Installed with an emergency safety parachute for the entire machine.
Low manufacturing and operating costs: The overall manufacturing cost is low, making it easy to mass produce and popularize. It can be fueled with 95 # gasoline, with a fuel consumption of 6-8 liters per 100 kilometers. The pilot's license is cheap, and the aircraft maintenance is simple and affordable, with strong compatibility.
Short certification cycle: Two fixed wing aircraft have fast certification, which can quickly form a commercial closed loop, quickly seize the low altitude economic market, and balance the characteristics of traditional aircraft and eVTOL, allowing for smooth operation.