Engineering:Salmson-Béchereau SB-2
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Short description: Trainer aircraft built by Salmson
| Salmson-Béchereau SB-2 | |
|---|---|
| Role | Two seat trainer aircraft |
| National origin | France |
| Manufacturer | Salmson |
| Designer | Louis Béchereau |
| First flight | 1923 |
| Number built | 1 |
| Variants | Salmson-Béchereau SB-3 |
The Salmson-Béchereau SB-2 was a trainer aircraft built by the France company Salmson.
The SB-2 was basically a mid-wing monoplane design. Only one aircraft was built.
Specifications
Data from [1]
General characteristics
- Crew: One
- Length: 6.03 m (19 ft 9 in)
- Wingspan: 7.0 m (23 ft 0 in)
- Height: 2.14 m (7 ft 0 in)
- Wing area: 11 m2 (120 sq ft)
- Empty weight: 622 kg (1,371 lb)
- Powerplant: 1 × Salmson 9Ac 9 cylinder, water-cooled radial engine, 89 kW (120 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 220 km/h (140 mph, 120 kn)
References
- ↑ "Salmson-Béchereau SB-2 - avion d'entrainement - Un siècle d'aviation française". Aviafrance.com. 2000-12-30. https://www.aviafrance.com/salmson-bechereau-sb-2-aviation-france-9039.htm. Retrieved 2022-08-31.
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