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 |