Engineering:SELA monoplane
From HandWiki
| SELA monoplane | |
|---|---|
| Role | Monoplane |
| National origin | France |
| Manufacturer | Société d'Etude pour la Locomotion Aérienne (SELA) |
| Number built | 1 |
The SELA monoplane was an experimental monoplane built by Société d'Etude pour la Locomotion Aérienne (SELA) in the early 1910s. It was a middle-wing monoplane similar in layout to the Bleriot monoplanes.
Specifications
Data from [1]
General characteristics
- Crew: 1
- Length: 8.80 m (28 ft 10 in)
- Wingspan: 11.20 m (36 ft 9 in)
- Gross weight: 420 kg (926 lb)
- Powerplant: 1 × SELA V-8 V-8 air-cooled piston engine, 63 kW (85 hp)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 116 km/h (72 mph, 63 kn)
References
- ↑ Bruno Parmentier. "Avions SELA - Aviation française". https://www.aviafrance.com/constructeur.php?ID_CONSTRUCTEUR=1522. Retrieved 2019-03-02.
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