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FlytCycle
The FlytCycle is a Wingless eVTOL aircraft developed by Flyt Aerospace in San Jose, United States. It is currently in the Scaled Prototype phase. Its first manned flight test was carried out in July 2017. The FlytCycle aircraft has a capacity of one (1) occupant. For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | FlytCycle |
Company | Flyt Aerospace |
Industry | Start-ups |
City | San Jose |
Country | United States |
Primary Classification | Wingless |
Secondary Classification | |
Tertiary Classification | Multicopter |
Energy Source | Battery |
Capacity | 1 seat |
Pilot type | Piloted |
Announced | July 2017 |
First (Unmanned) Flight | |
First (Manned) Flight | 2017-07-14 |
Design Maturity | Scaled Prototype |
Official Website | http://flytaerospace.com/ |
Geometry | |
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Length | |
Height | |
Span | |
Wing Configuration | |
Wing sweep? |
Seating | |
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|
|
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) | 238 kg |
Operating Empty Weight (OEW) | 75 kg |
Payload | 104 kg |
Battery Mass | 59 kg |
Cruise Speed | |
Max Speed | |
Range | |
Endurance | |
Cruise Altitude | |
Max Altitude | |
Thrust | |
Power Available |
Propulsors | |
---|---|
Propulsor Type | Prop |
Propulsor Layout | |
Total Number of Propulsors | 6 |
Propulsors in Cruise | |
Propulsor in Hover | 6 |
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? | No |
Independent Ground Taxi? | |
Conventional Landing? | |
Amphibious? |