Spirit | 19 | 25 | 27 | 29 | |
2006 | 2005 | 2005 | 2005 | ||
In-Flight-Weight | kg | 55 - 85 | 80 - 100 | 95 - 115 | |
Main-Use | Cross | Cross | Cross | Cross | |
Certifications | |||||
Naked-Pilot | kg | 52 | 71 | 85 | |
Wing-Load | kg/m² | 2,8 | 3,4 | 3,6 | |
Wing-Weight | |||||
Area | m² | 19,0 | 24,7 | 26,8 | 29,0 |
Area proj | |||||
Span | m | 10,5 | 12,0 | 12,5 | 13,0 |
Span proj | |||||
Ratio | 5,9 | 5,9 | 5,9 | 5,9 | |
Ratio proj | |||||
Rows | |||||
Boxes | 21 | 21 | 21 | 21 | |
Cells | 55 | 55 | 55 | 55 | |
Closed Cells | 8 | 8 | 8 | 8 | |
Lines Ø diam. | |||||
Lines distance | |||||
Lines total | |||||
Flattening | |||||
Accelerated speed | |||||
Basic speed | |||||
Minimum speed | |||||
Best-Sink-Rate | m/s | 1,1 | 1,1 | 1,1 | 1,1 |
Best-Glide-Ratio | 1,2 m/s - 37 km/h | 1,2 m/s - 37 km/h | 1,2 m/s - 37 km/h | 1,2 m/s - 37 km/h | |
GR/Fmax Estimations | 8,5 - 8,8 | 8,5 - 8,8 | 8,5 - 8,8 | 8,5 - 8,8 | |
Upper-Surface | |||||
Under-Surface | |||||
Lines type | |||||
Risers | |||||
Accelerator | |||||
Trims | |||||
Ears | |||||
B Lines |