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Technische Daten
| Bristell B23 | |
| Dimensions | |
| Wing span | 9,274 m |
| Wing area | 11,75 m2 |
| Wing loading | 63,82 kg/m2 |
| Aircraft length | 6,585 m |
| Aircraft height | 2,36 m |
| Cabin width | 1,30 m |
| Weights | |
| Empty weight | 450 kg |
| Maximum take-off weight (MTOW) | 750 kg |
| Useful load | 300 kg |
| Fuel tanks capacity | 120 l |
| Fuselage luggage compartment | 15 kg |
| Wing luggage compartment | 2 x 20 kg |
| Load factor | +4/-2 g |
| Operational Speed | |
| Stall speed with flaps VSO | |
| Stall speed without flaps VS1 | |
| Manoeuvring speed VA | |
| Maximum flap speed VFE | |
| Maximum horizontal flight speed VH | |
| Never exceeded speed VNE | |
| Power Units | |
| ROTAX 912 UL | |
| ROTAX 912 ULS | |
| ROTAX 912 iS sport | |
| ROTAX 914 UL | |
| ROTAX 915 iS |
