Paraglider
◄ | Stewart | 41 | |
| 2015 | ||
| In-Flight-Weight | kg | 125 - 220 |
| Main-Use | Tandem | |
| Certifications | ; | |
| Naked-Pilot | kg | 95 - 190 |
| Wing-Load | kg/m² | 3,1 - 5,4 |
| Wing-Weight | ||
| Area | m² | 40,90 |
| Area proj | ||
| Span | m | 14,86 |
| Span proj | ||
| Ratio | 5,40 | |
| Ratio proj | ||
| Rows | 4 | |
| Boxes | 21 | |
| Cells | 53 | |
| Closed Cells | 10 | |
| Lines Ø diam. | ||
| Lines distance | m | 8,39 |
| Lines total | ||
| Flattening | ||
| Accelerated speed | km/h | 50 |
| Basic speed | km/h | 40 |
| Minimum speed | ||
| Best-Sink-Rate | ||
| Best-Glide-Ratio | ||
| GR/Fmax Estimations | ||
| Upper-Surface | ||
| Under-Surface | ||
| Lines type | ||
| Risers | 5(2A+1A'/3B/4C/2D) | |
| Accelerator | No | |
| Trims | Yes | |
| Ears | Yes | |
| B Lines | Yes |
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