Roadable PAV configuration (baseline)
| PAV Configuration (baseline) | |
|---|---|
| PAV material | Composite |
| Wing airfoil | FX 63–137 |
| Trailing edge high lift device | Single slotted flap |
| Wing morphing | Folding-rotating |
| Propulsion type | Propeller |
| Propeller blade number | 3 |
| Fuselage length/width/height | 17 ft/6 ft/5 ft |
| Main wing aspect ratio | 7.6 |
| Horizontal tail volume coefficient/aspect ratio/taper ratio | 0.7/3/0.5 |
| Vertical tail volume coefficient/aspect ratio/taper ratio | 0.04/1/0.6 |
| Composite | |
| FX 63–137 | |
| Single slotted flap | |
| Folding-rotating | |
| Propeller | |
| 3 | |
| 17 ft/6 ft/5 ft | |
| 7.6 | |
| 0.7/3/0.5 | |
| 0.04/1/0.6 | |
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