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Pop.Up
The Pop.Up is a Wingless eVTOL aircraft developed by Airbus, Italdesign & Audi in Toulouse, France. It is currently in the Initial Design phase. The Pop.Up aircraft has a capacity of two (2) occupants. and a range of 60 units. For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | Pop.Up |
Company | Airbus, Italdesign & Audi |
Industry | Major aerospace |
City | Toulouse |
Country | France |
Primary Classification | Wingless |
Secondary Classification | |
Tertiary Classification | Multicopter |
Energy Source | Battery |
Capacity | 2 seats |
Pilot type | Autonomous |
Announced | March 2017 |
First (Unmanned) Flight | |
First (Manned) Flight | |
Design Maturity | Initial Design |
Official Website | https://www.italdesign.it/project/pop-up-next/ |
Geometry | |
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Length | |
Height | |
Span | |
Wing Configuration | |
Wing sweep? |
Seating | |
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|
|
Seating Configuration | 1x2 |
Passenger Seat Rows | 1 seat |
Seats per Row | 2 seats |
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 | |
Max Speed | 68 kt |
Range | 32.4 nm |
Endurance | |
Cruise Altitude | |
Max Altitude | |
Thrust | |
Power Available | 480 kW |
Propulsors | |
---|---|
Propulsor Type | Fan |
Propulsor Layout | |
Total Number of Propulsors | 8 |
Propulsors in Cruise | |
Propulsor in Hover | 8 |
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 | 15 min |
Battery Charge Rate | |
Charging Voltage |
Maneuverability | |
---|---|
Wheeled Ground Taxi? | Yes |
Independent Ground Taxi? | Yes |
Conventional Landing? | |
Amphibious? |