Thesis | 60 | 80 | 100 | |
2005 | 2005 | 2005 | ||
In-Flight-Weight | kg | 60 - 85 | 80 - 105 | 100 - 125 |
Main-Use | Initiation | Initiation | Initiation | |
Certifications | ||||
Naked-Pilot | kg | 57 | 76 | 95 |
Wing-Load | kg/m² | 2,8 | 3,3 | 3,7 |
Wing-Weight | kg | 5,2 | 5,5 | 5,9 |
Area | m² | 25,7 | 27,9 | 30,1 |
Area proj | m² | 22,3 | 24,2 | 26,1 |
Span | m | 10,8 | 11,2 | 11,7 |
Span proj | m | 8,6 | 9,0 | 9,4 |
Ratio | 4,5 | 4,5 | 4,5 | |
Ratio proj | 3,4 | 3,4 | 3,4 | |
Rows | 4 | 4 | 4 | |
Boxes | 37 | 37 | 37 | |
Cells | 40 | 40 | 40 | |
Closed Cells | 10 | 10 | 10 | |
Lines Ø diam. | ||||
Lines distance | 7,53 m | |||
Lines total | ||||
Flattening | % | 13 | 13 | 13 |
Accelerated speed | km/h | 46 | 46 | 46 |
Basic speed | km/h | 37 | 37 | 37 |
Minimum speed | km/h | 22 | 22 | 22 |
Best-Sink-Rate | m/s | 1,2 | 1,2 | 1,2 |
Best-Glide-Ratio | 1,3 m/s - 36 km/h | 1,3 m/s - 36 km/h | 1,3 m/s - 36 km/h | |
GR/Fmax Estimations | 7,5 - 7,8 | 7,5 - 7,8 | 7,5 - 7,8 | |
Upper-Surface | S9017-E77A 40 g/m² | S9017-E77A 40 g/m² | S9017-E77A 40 g/m² | |
Under-Surface | S9017-E38A 40 g/m² | S9017-E38A 40 g/m² | S9017-E38A 40 g/m² | |
Lines type | Dyneema; Aramid | Dyneema; Aramid | Dyneema; Aramid | |
Risers | 4(3A/3B/3C/3D) | 4(3A/3B/3C/3D) | 4(3A/3B/3C/3D) | |
Accelerator | Yes | Yes | Yes | |
Trims | No | No | No | |
Ears | m/s | 3 | 3 | 3 |
B Lines | m/s | 8 | 8 | 8 |