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Napoleon Aero VTOL

The Napoleon Aero VTOL is a Powered Lift eVTOL aircraft developed by Napoleon Aero in Moscow, Russia. It is currently in the Initial Design phase. The Napoleon Aero VTOL aircraft has a capacity of four (4) occupants. and a range of 100 units.

Last updated on February 26th, 2024.

Characteristics

General
Name	Napoleon Aero VTOL
Company	Napoleon Aero
Industry	Start-ups
City	Moscow
Country	Russia
Primary Classification	Powered Lift
Secondary Classification	Separate Thrust
Tertiary Classification	Lift + Cruise
Energy Source	Battery
Capacity	4 seats
Pilot type	Piloted
Announced	December 2017
First (Unmanned) Flight
First (Manned) Flight
Design Maturity	Initial Design
Official Website

Geometry
Length
Height
Span
Wing Configuration
Wing sweep?

Seating

Seating Configuration	4 seat
Passenger Seat Rows
Seats per Row
Separated pilot seat?	Yes
Seating Layout	Standard

Performance
Max Take-off Weight (MTOW)	1360 kg
Operating Empty Weight (OEW)
Payload	400 kg
Battery Mass
Cruise Speed
Max Speed
Range	54 nm
Endurance
Cruise Altitude
Max Altitude
Thrust
Power Available

Propulsors
Propulsor Type	Fan
Propulsor Layout
Total Number of Propulsors	47
Propulsors in Cruise	1
Propulsor in Hover	46
Individual Propulsor Thrust
Individual Propulsor Power

Electric Energy
Battery Capacity
Battery Power
Battery Density
Battery Current
Battery Voltage
Battery Chemical System
Battery Charge Time
Battery Charge Rate
Charging Voltage

Maneuverability
Wheeled Ground Taxi?	Yes
Independent Ground Taxi?
Conventional Landing?
Amphibious?