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PAC VTOL 720-200
The PAC VTOL 720-200 is a Powered Lift eVTOL aircraft developed by Flyter in Moscow, Russia. It is currently in the Initial Design phase. The PAC VTOL 720-200 aircraft has a capacity of two (2) occupants. It also has a cruise speed of 250 units, and a range of 900 units. For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | PAC VTOL 720-200 |
Company | Flyter |
Industry | Start-ups |
City | Moscow |
Country | Russia |
Primary Classification | Powered Lift |
Secondary Classification | Separate Thrust |
Tertiary Classification | Lift + Cruise |
Energy Source | Hybrid-Electric |
Capacity | 2 seats |
Pilot type | Piloted |
Announced | April 2019 |
First (Unmanned) Flight | |
First (Manned) Flight | |
Design Maturity | Initial Design |
Official Website | https://flyter.aero/ |
Geometry | |
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Length | 6.3 m |
Height | 2.7 m |
Span | 7 m |
Wing Configuration | Canard |
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) | |
Operating Empty Weight (OEW) | |
Payload | |
Battery Mass | |
Cruise Speed | 135 kt |
Max Speed | 162 kt |
Range | 486 nm |
Endurance | |
Cruise Altitude | |
Max Altitude | 9842 m |
Thrust | |
Power Available |
Propulsors | |
---|---|
Propulsor Type | Prop |
Propulsor Layout | |
Total Number of Propulsors | 9 |
Propulsors in Cruise | 1 |
Propulsor in Hover | 8 |
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? |