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aEro 2
The aEro 2 is a Powered Lift eVTOL aircraft developed by Dufour Aerospace in Zurich, Switzerland. It is currently in the Scaled Prototype phase. The aEro 2 aircraft has a capacity of two (2) occupants. It also has a cruise speed of 320 units, and a range of 120 units. For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | aEro 2 |
Company | Dufour Aerospace |
Industry | Start-ups |
City | Zurich |
Country | Switzerland |
Primary Classification | Powered Lift |
Secondary Classification | Vectored Thrust |
Tertiary Classification | Tilt Wing |
Energy Source | Battery |
Capacity | 2 seats |
Pilot type | Piloted |
Announced | March 2018 |
First (Unmanned) Flight | |
First (Manned) Flight | |
Design Maturity | Scaled Prototype |
Official Website | http://dufour.aero/ |
Geometry | |
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Length | |
Height | |
Span | |
Wing Configuration | Conventional |
Wing sweep? |
Seating | |
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|
|
Seating Configuration | 2x1 |
Passenger Seat Rows | 2 seats |
Seats per Row | 1 seat |
Separated pilot seat? | |
Seating Layout | Standard |
Performance | |
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Max Take-off Weight (MTOW) | |
Operating Empty Weight (OEW) | |
Payload | |
Battery Mass | |
Cruise Speed | 172.8 kt |
Max Speed | |
Range | 64.8 nm |
Endurance | |
Cruise Altitude | |
Max Altitude | |
Thrust | |
Power Available |
Propulsors | |
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Propulsor Type | Prop |
Propulsor Layout | |
Total Number of Propulsors | 2 |
Propulsors in Cruise | 2 |
Propulsor in Hover | 2 |
Individual Propulsor Thrust | |
Individual Propulsor Power |
Electric Energy | |
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Battery Capacity | |
Battery Power | |
Battery Density | |
Battery Current | 0.00 |
Battery Voltage | |
Battery Chemical System | |
Battery Charge Time | |
Battery Charge Rate | |
Charging Voltage |
Maneuverability | |
---|---|
Wheeled Ground Taxi? | Yes |
Independent Ground Taxi? | |
Conventional Landing? | Yes |
Amphibious? |