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J2000
The J2000 is a Powered Lift eVTOL aircraft developed by Jetoptera in Dallas, United States. It is currently in the Scaled Prototype phase. The J2000 aircraft has a capacity of two (2) occupants. It also has a cruise speed of 322 units, and a range of 322 units. For more information on this aircraft, see their website.
Last updated on February 26th, 2024.
Characteristics
General | |
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Name | J2000 |
Company | Jetoptera |
Industry | Start-ups |
City | Dallas |
Country | United States |
Primary Classification | Powered Lift |
Secondary Classification | Vectored Thrust |
Tertiary Classification | Tilt Fan |
Energy Source | Hybrid-Electric |
Capacity | 2 seats |
Pilot type | Piloted |
Announced | May 2018 |
First (Unmanned) Flight | |
First (Manned) Flight | |
Design Maturity | Scaled Prototype |
Official Website | http://www.jetoptera.com/ |
Geometry | |
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Length | |
Height | |
Span | |
Wing Configuration | Box |
Wing sweep? | No |
Seating | |
---|---|
|
|
Seating Configuration | 2 seat |
Passenger Seat Rows | |
Seats per Row | |
Separated pilot seat? | Yes |
Seating Layout | Standard |
Performance | |
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Max Take-off Weight (MTOW) | 907 kg |
Operating Empty Weight (OEW) | |
Payload | 181 kg |
Battery Mass | |
Cruise Speed | 173.8 kt |
Max Speed | |
Range | 173.9 nm |
Endurance | |
Cruise Altitude | |
Max Altitude | 15000 m |
Thrust | 8.9 kN |
Power Available |
Propulsors | |
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Propulsor Type | Fan |
Propulsor Layout | |
Total Number of Propulsors | 4 |
Propulsors in Cruise | 2 |
Propulsor in Hover | 4 |
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? | Yes |
Amphibious? |