| Cobra | XS | S | M | L | |
| 2009 | 2009 | 2009 | 2009 | ||
| In-Flight-Weight | kg | 65 - 75 | 70 - 85 | 85 - 105 | 95 - 125 |
| Main-Use | Cross | Cross | Cross | Cross | |
| Certifications | ; | ; | ; | ; | |
| Naked-Pilot | kg | 52 | 59 | 75 | 89 |
| Wing-Load | kg/m² | 3,1 | 3,3 | 3,9 | 4,2 |
| Wing-Weight | |||||
| Area | m² | 22,5 | 23,5 | 24,5 | 26,1 |
| Area proj | m² | 19,1 | 20,0 | 20,8 | 22,2 |
| Span | m | 12,1 | 12,3 | 12,6 | 13,5 |
| Span proj | |||||
| Ratio | 6,6 | 6,6 | 6,6 | 6,6 | |
| Ratio proj | |||||
| Rows | |||||
| Boxes | |||||
| Cells | |||||
| Closed Cells | |||||
| Lines Ø diam. | |||||
| Lines distance | |||||
| Lines total | |||||
| Flattening | % | 15 | 15 | 15 | 15 |
| Accelerated speed | km/h | 60 | 60 | 60 | 60 |
| Basic speed | |||||
| Minimum speed | km/h | 22 | 22 | 22 | 22 |
| Best-Sink-Rate | |||||
| Best-Glide-Ratio | |||||
| GR/Fmax Estimations | p | 10,0 | 10,0 | 10,0 | 10,0 |
| Upper-Surface | |||||
| Under-Surface | |||||
| Lines type | Kevlar | Kevlar | Kevlar | Kevlar | |
| Risers | 3 | 3 | 3 | 3 | |
| Accelerator | Yes | Yes | Yes | Yes | |
| Trims | No | No | No | No | |
| Ears | m/s | 3 | 3 | 3 | 3 |
| B Lines | m/s | 6 | 6 | 6 | 6 |