Nazzeni eVTOL aircraft CR-900 its an Hybrid (Li-ion + H₂) hydrogen electric vertical take-off and landing aircraft, with cargo transportation package

Flight characteristics:

Number of seats- 1 , 1 pilot
Maximum distance — 350 km
Maximum altitude -2000 meter
Maximum speed -295 km/h
Maximum fly time — 60 minutes
Maximum payload — 500 kg
Maximum payload volume -4 cbm
Emty weight — 1100 kg
Maximum takeoff weight- 1600 kg
Sizes L-6710, W-5247, H-2762 mm

Technical parametrs

Main structure — carbon fiber
Hybrid battary sistem (Li-ion + H₂) weight — 390 kg
Volume of the cylinder 100 liters
Mass of H₂-system 189 kg
Flight duration 59 min
Total mass 1526.5 kg
Energy capacity 26.55 kW·h
Maximum power 675 kW
Power of the fuel cell element is 100 kW
Mass of hydrogen 4.0 kg
Presure 700 bar
Quantity of EDF engines: 30 piece
Engine power (total) 675 kW