TAS-102 Specifications and Performance
Specifications1
| 1 | All specifications are design estimates. | |
| 2 | Derived from conceptual design and engineering analysis. | |
| 3 | Listed takeoff and landing distances are calculated using standard aircraft design parameters and do not reflect the use of the vehicle's motorcycle engine and brakes. The use of a separate engine for power directly to the rear wheel, along with increased braking power, will significantly reduce this vehicle's runway distance requirements. |