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Aurora PAV
The Aurora PAV is a Powered Lift eVTOL aircraft developed by Boeing in Washington, United States. It is currently in the Scaled Prototype phase. Its first manned flight test was carried out in January 2019. The Aurora PAV aircraft has a capacity of two (2) occupants. It also has a cruise speed of 180 units, For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | Aurora PAV |
Company | Boeing |
Industry | Major aerospace |
City | Washington |
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 | April 2017 |
First (Unmanned) Flight | |
First (Manned) Flight | 2019-01-23 |
Design Maturity | Scaled Prototype |
Official Website | http://www.aurora.aero/evtol/ |
Geometry | |
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Length | 8 m |
Height | |
Span | 8 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) | 800 kg |
Operating Empty Weight (OEW) | 575 kg |
Payload | 225 kg |
Battery Mass | |
Cruise Speed | 97.2 kt |
Max Speed | |
Range | |
Endurance | |
Cruise Altitude | |
Max Altitude | |
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? |