Sora | 41 | |
2014 | ||
In-Flight-Weight | kg | 120 - 220 |
Main-Use | Tandem | |
Certifications | ||
Naked-Pilot | kg | 90 - 190 |
Wing-Load | kg/m² | 2,9 - 5,4 |
Wing-Weight | kg | 7,5 |
Area | m² | 41,00 |
Area proj | m² | 35,10 |
Span | m | 14,90 |
Span proj | m | 11,70 |
Ratio | 5,35 | |
Ratio proj | 3,90 | |
Rows | 4 | |
Boxes | 25 | |
Cells | 54 | |
Closed Cells | 10 | |
Lines Ø diam. | 3,0 mm; 2,0 mm; 1,4 mm; 1,1 mm | |
Lines distance | m | 8,59 |
Lines total | ||
Flattening | % | 14 |
Accelerated speed | km/h | 52 |
Basic speed | ||
Minimum speed | km/h | 25 |
Best-Sink-Rate | ||
Best-Glide-Ratio | ||
GR/Fmax Estimations | ||
Upper-Surface | S9017-E25 38 g/m² | |
Under-Surface | S70032-E3W 32 g/m² | |
Lines type | Liros; Edelrid | |
Risers | 5(2A+1A'/4B/3C/2D) | |
Accelerator | No | |
Trims | 15 | |
Ears | Yes | |
B Lines | No |