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FlyKart 2
The FlyKart 2 is a Wingless eVTOL aircraft developed by Trek Aerospace in Sacramento, United States. It is currently in the Initial Design phase. The FlyKart 2 aircraft has a capacity of one (1) occupant. It also has a cruise speed of 83 units, For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | FlyKart 2 |
Company | Trek Aerospace |
Industry | Start-ups |
City | Sacramento |
Country | United States |
Primary Classification | Wingless |
Secondary Classification | |
Tertiary Classification | Multicopter |
Energy Source | Battery |
Capacity | 1 seat |
Pilot type | Piloted |
Announced | June 2018 |
First (Unmanned) Flight | |
First (Manned) Flight | |
Design Maturity | Initial Design |
Official Website | https://www.trekaero.com/ |
Geometry | |
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Length | 2 m |
Height | 1.2 m |
Span | 2 m |
Wing Configuration | |
Wing sweep? |
Seating | |
---|---|
|
|
Seating Configuration | 1 seat |
Passenger Seat Rows | |
Seats per Row | |
Separated pilot seat? | Yes |
Seating Layout | Standard |
Performance | |
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Max Take-off Weight (MTOW) | |
Operating Empty Weight (OEW) | |
Payload | |
Battery Mass | |
Cruise Speed | 44.8 kt |
Max Speed | 55.1 kt |
Range | |
Endurance | 30 min |
Cruise Altitude | |
Max Altitude | |
Thrust | |
Power Available |
Propulsors | |
---|---|
Propulsor Type | Fan |
Propulsor Layout | |
Total Number of Propulsors | 10 |
Propulsors in Cruise | 10 |
Propulsor in Hover | 10 |
Individual Propulsor Thrust | |
Individual Propulsor Power |
Electric Energy | |
---|---|
Battery Capacity | 9.6 Kwh |
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? | |
Independent Ground Taxi? | |
Conventional Landing? | |
Amphibious? |