| Hercules | 380 | |
| 2016 | ||
| In-Flight-Weight | kg | 180 - 380 |
| Main-Use | Paramotor | |
| Certifications | ||
| Naked-Pilot | kg | 120 - 320 |
| Wing-Load | kg/m² | 4,7 - 9,9 |
| Wing-Weight | kg | 9,5 |
| Area | m² | 38,36 |
| Area proj | m² | 33,43 |
| Span | m | 14,20 |
| Span proj | m | 11,53 |
| Ratio | 5,26 | |
| Ratio proj | 3,97 | |
| Rows | 4 | |
| Boxes | 29 | |
| Cells | 42 | |
| Closed Cells | 8 | |
| Lines Ø diam. | 2,5 mm; 2,1 mm; 1,5 mm; 1,0 mm | |
| Lines distance | ||
| Lines total | ||
| Flattening | % | 13 |
| Accelerated speed | 65 km/h; 60 km/h | |
| Basic speed | km/h | 52 |
| Minimum speed | km/h | 32 |
| Best-Sink-Rate | m/s | 1,4 |
| Best-Glide-Ratio | ||
| GR/Fmax Estimations | p | 8,0 |
| Upper-Surface | Gelv. WTX 40 g/m² | |
| Under-Surface | Gelv. WTX 40 g/m² | |
| Lines type | Technora; Vectran | |
| Risers | 4(4A/5B/4C/4D) | |
| Accelerator | Yes | |
| Trims | Yes | |
| Ears | Yes | |
| B Lines | Yes |