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ZeroG
The ZeroG is a Wingless eVTOL aircraft developed by Davinci Technology in Hanoi, Vietnam. It is currently in the Scaled Prototype phase. Its first manned flight test was carried out in November 2017. The ZeroG 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 | ZeroG |
Company | Davinci Technology |
Industry | Start-ups |
City | Hanoi |
Country | Vietnam |
Primary Classification | Wingless |
Secondary Classification | |
Tertiary Classification | Multicopter |
Energy Source | Battery |
Capacity | 1 seat |
Pilot type | Piloted |
Announced | January 2017 |
First (Unmanned) Flight | |
First (Manned) Flight | 2017-11-04 |
Design Maturity | Scaled Prototype |
Official Website | http://da-vinci.us/ |
Geometry | |
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Length | |
Height | |
Span | |
Wing Configuration | |
Wing sweep? |
Seating | |
---|---|
|
|
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) | 240 kg |
Operating Empty Weight (OEW) | 90 kg |
Payload | 150 kg |
Battery Mass | 50 kg |
Cruise Speed | |
Max Speed | 38 kt |
Range | |
Endurance | 25 min |
Cruise Altitude | |
Max Altitude | |
Thrust | |
Power Available |
Propulsors | |
---|---|
Propulsor Type | Fan |
Propulsor Layout | |
Total Number of Propulsors | 6 |
Propulsors in Cruise | 6 |
Propulsor in Hover | 6 |
Individual Propulsor Thrust | |
Individual Propulsor Power |
Electric Energy | |
---|---|
Battery Capacity | 52.8 Kwh |
Battery Power | |
Battery Density | 1056.00 |
Battery Current | 1191.00 |
Battery Voltage | |
Battery Chemical System | Lithium-polymer |
Battery Charge Time | |
Battery Charge Rate | |
Charging Voltage | 25.20 |
Maneuverability | |
---|---|
Wheeled Ground Taxi? | No |
Independent Ground Taxi? | |
Conventional Landing? | |
Amphibious? |