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Pegasus
The Pegasus is a eVTOL aircraft developed by Supervolant in Mannheim, Germany. It is currently in the Initial Design phase. The Pegasus aircraft has a capacity of two (2) occupants. and a range of 1852 units.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | Pegasus |
Company | Supervolant |
Industry | Start-ups |
City | Mannheim |
Country | Germany |
Primary Classification | |
Secondary Classification | |
Tertiary Classification | |
Energy Source | Hybrid-Electric |
Capacity | 2 seats |
Pilot type | |
Announced | May 2018 |
First (Unmanned) Flight | |
First (Manned) Flight | |
Design Maturity | Initial Design |
Official Website |
Geometry | |
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Length | |
Height | |
Span | |
Wing Configuration | Canard |
Wing sweep? | Yes |
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 | 330 kt |
Range | 1000 nm |
Endurance | |
Cruise Altitude | |
Max Altitude | 29000 m |
Thrust | |
Power Available |
Propulsors | |
---|---|
Propulsor Type | Fan |
Propulsor Layout | |
Total Number of Propulsors | 4 |
Propulsors in Cruise | |
Propulsor in Hover | 4 |
Individual Propulsor Thrust | |
Individual Propulsor Power |
Electric Energy | |
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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? | |
Independent Ground Taxi? | |
Conventional Landing? | |
Amphibious? |