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Y6S
The Y6S is a Powered Lift eVTOL aircraft developed by Autonomous Flight in London, United Kingdom. It is currently in the Initial Design phase. The Y6S aircraft has a capacity of two (2) occupants. and a range of 129 units. For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | Y6S |
Company | Autonomous Flight |
Industry | Start-ups |
City | London |
Country | United Kingdom |
Primary Classification | Powered Lift |
Secondary Classification | Combined Vectored Thrust |
Tertiary Classification | Tilt Wing |
Energy Source | Battery |
Capacity | 2 seats |
Pilot type | Autonomous |
Announced | January 2018 |
First (Unmanned) Flight | |
First (Manned) Flight | |
Design Maturity | Initial Design |
Official Website | http://autonomousflight.com/ |
Geometry | |
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Length | |
Height | |
Span | |
Wing Configuration | Canard |
Wing sweep? |
Seating | |
---|---|
|
|
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 | 60 kt |
Range | 69.7 nm |
Endurance | |
Cruise Altitude | |
Max Altitude | 1500 m |
Thrust | |
Power Available |
Propulsors | |
---|---|
Propulsor Type | Fan |
Propulsor Layout | |
Total Number of Propulsors | 3 |
Propulsors in Cruise | 2 |
Propulsor in Hover | 3 |
Individual Propulsor Thrust | |
Individual Propulsor Power |
Electric Energy | |
---|---|
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? | No |
Independent Ground Taxi? | |
Conventional Landing? | |
Amphibious? |