Blériot-SPAD S.39
| SPAD S.39 | |
|---|---|
| |
| Role | Reconnaissance aircraft |
| National origin | France |
| Manufacturer | SPAD |
| First flight | 1 June 1921 |
| Number built | 2 |
The Bleriot-SPAD S.39 was a French carrier-borne reconnaissance aircraft built in the early 1920s.
Design[edit]
The S.39 was a biplane with monocoque fuselage and wood and canvas wings. The undercarriage featured a hydroplane / flotation device.
Specifications[edit]
Data from [1]
General characteristics
- Crew: 2
- Length: 7.83 m (25 ft 8 in)
- Wingspan: 10.43 m (34 ft 3 in)
- Height: 2.93 m (9 ft 7 in)
- Wing area: 33.00 m2 (355.2 sq ft)
- Empty weight: 1,028 kg (2,266 lb)
- Gross weight: 1,520 kg (3,351 lb)
- Powerplant: 1 × Hispano-Suiza , 205 kW (275 hp)
- Propellers: 2-bladed fixed pitchpropeller
Performance
- Maximum speed: 220 km/h (140 mph, 120 kn)
See also[edit]
Related lists
References[edit]
Wikimedia Commons has media related to Blériot-SPAD S.39.
- ^ "SPAD S-39 - avion de reconnaissance - Un siècle d'aviation française". Aviafrance.com. Retrieved 2019-02-04.