Thrust | S | M | L | XL | |
2005 | 2004 | 2004 | 2004 | ||
In-Flight-Weight | kg | 70 - 115 | 85 - 135 | 100 - 155 | 110 - 180 |
Main-Use | Paramotor | Paramotor | Paramotor | Paramotor | |
Certifications | |||||
Naked-Pilot | kg | 54 - 99 | 68 - 118 | 82 - 137 | 91 - 161 |
Wing-Load | kg/m² | 2,6 - 4,2 | 2,9 - 4,6 | 3,2 - 5,0 | 3,3 - 5,4 |
Wing-Weight | kg | 6,5 | 6,9 | 7,3 | 7,6 |
Area | m² | 27,30 | 29,30 | 31,30 | 33,30 |
Area proj | m² | 23,40 | 25,20 | 26,90 | 28,60 |
Span | m | 11,58 | 12,20 | 12,90 | 13,50 |
Span proj | m | 9,32 | 9,85 | 10,40 | 10,90 |
Ratio | 4,91 | 5,08 | 5,31 | 5,47 | |
Ratio proj | 3,71 | 3,85 | 4,02 | 4,15 | |
Rows | 4 | 4 | 4 | 4 | |
Boxes | 25 | 27 | 29 | 31 | |
Cells | 42 | 44 | 46 | 48 | |
Closed Cells | 6 | 6 | 6 | 6 | |
Lines Ø diam. | 1,9 mm; 1,8 mm; 1,5 mm; 1,1 mm | 1,9 mm; 1,8 mm; 1,5 mm; 1,1 mm | 1,9 mm; 1,8 mm; 1,5 mm; 1,1 mm | 1,9 mm; 1,8 mm; 1,5 mm; 1,1 mm | |
Lines distance | m | 6,60 | 7,00 | 7,40 | 7,70 |
Lines total | m | 407 | 421 | 441 | 481 |
Flattening | % | 14 | 14 | 14 | 14 |
Accelerated speed | 50 km/h; 45 km/h | 50 km/h; 45 km/h | 50 km/h; 45 km/h | 50 km/h; 45 km/h | |
Basic speed | km/h | 37 | 37 | 37 | 37 |
Minimum speed | km/h | 21 | 21 | 21 | 21 |
Best-Sink-Rate | m/s | 1,1 | 1,1 | 1,1 | 1,1 |
Best-Glide-Ratio | 1,2 m/s - 35 km/h | 1,2 m/s - 35 km/h | 1,2 m/s - 35 km/h | 1,2 m/s - 35 km/h | |
GR/Fmax Estimations | 7,9 - 8,2 | 7,9 - 8,2 | 7,9 - 8,2 | 7,9 - 8,2 | |
Upper-Surface | Gelvenor 46 g/m² | Gelvenor 46 g/m² | Gelvenor 46 g/m² | Gelvenor 46 g/m² | |
Under-Surface | Gelvenor 46 g/m² | Gelvenor 46 g/m² | Gelvenor 46 g/m² | Gelvenor 46 g/m² | |
Lines type | SuperAramid; Dyneema | SuperAramid; Dyneema | SuperAramid; Dyneema | SuperAramid; Dyneema | |
Risers | 5(2A+1A'/4B/3C/3D) | 5(2A+1A'/4B/3C/3D) | 5(2A+1A'/4B/3C/3D) | 5(2A+1A'/4B/3C/3D) | |
Accelerator | cm | 20 | 20 | 20 | 20 |
Trims | Yes | Yes | Yes | Yes | |
Ears | 3m/s | 3m/s | 3m/s | 3m/s | |
B Lines | 7m/s | 7m/s | 7m/s | 7m/s |