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teTra 3
The teTra 3 is a Wingless eVTOL aircraft developed by teTra in Tokyo, Japan. It is currently in the Initial Design phase. The teTra 3 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 | |
|---|---|
| Name | teTra 3 |
| Company | teTra |
| Industry | Start-ups |
| City | Tokyo |
| Country | Japan |
| Primary Classification | Wingless |
| Secondary Classification | |
| Tertiary Classification | Multicopter |
| Energy Source | Battery |
| Capacity | 1 seat |
| Pilot type | Piloted |
| Announced | June 2018 |
| First (Unmanned) Flight | |
| First (Manned) Flight | |
| Design Maturity | Initial Design |
| Official Website | https://www.tetra-gofly.com/ |
| Geometry | |
|---|---|
| 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 | |
|---|---|
| Max Take-off Weight (MTOW) | |
| Operating Empty Weight (OEW) | |
| Payload | |
| Battery Mass | |
| Cruise Speed | |
| Max Speed | |
| Range | |
| Endurance | |
| Cruise Altitude | |
| Max Altitude | |
| Thrust | |
| Power Available | |
| Propulsors | |
|---|---|
| Propulsor Type | Fan |
| Propulsor Layout | |
| Total Number of Propulsors | 2 |
| Propulsors in Cruise | 2 |
| Propulsor in Hover | 2 |
| Individual Propulsor Thrust | |
| Individual Propulsor Power | |
| Electric Energy | |
|---|---|
| Battery Capacity | |
| Battery Power | |
| Battery Density | |
| Battery Current | |
| Battery Voltage | |
| Battery Chemical System | |
| Battery Charge Time | |
| Battery Charge Rate | |
| Charging Voltage | |
| Maneuverability | |
|---|---|
| Wheeled Ground Taxi? | |
| Independent Ground Taxi? | |
| Conventional Landing? | |
| Amphibious? | |