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Cora
The Cora is a Powered Lift eVTOL aircraft developed by Kitty Hawk in Memphis, United States. It is currently in the Manned Flight Testing phase. Its first manned flight test was carried out in March 2018. The Cora aircraft has a capacity of two (2) occupants. and a range of 100 units. For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | Cora |
Company | Kitty Hawk |
Industry | Start-ups |
City | Memphis |
Country | United States |
Primary Classification | Powered Lift |
Secondary Classification | Separate Thrust |
Tertiary Classification | Lift + Cruise |
Energy Source | Battery |
Capacity | 2 seats |
Pilot type | Piloted |
Announced | March 2018 |
First (Unmanned) Flight | |
First (Manned) Flight | 2018-03-12 |
Design Maturity | Manned Flight Testing |
Official Website | https://cora.aero/ |
Geometry | |
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Length | |
Height | |
Span | 11 m |
Wing Configuration | Conventional |
Wing sweep? | No |
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) | 1224 kg |
Operating Empty Weight (OEW) | |
Payload | 181 kg |
Battery Mass | |
Cruise Speed | |
Max Speed | 97.2 kt |
Range | 54 nm |
Endurance | 19 min |
Cruise Altitude | |
Max Altitude | 3000 m |
Thrust | |
Power Available |
Propulsors | |
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Propulsor Type | Prop |
Propulsor Layout | |
Total Number of Propulsors | 13 |
Propulsors in Cruise | 1 |
Propulsor in Hover | 12 |
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? | |
Amphibious? |