Engineering:Blériot-SPAD S.36
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Short description: 1920s French aircraft
| SPAD S.36 | |
|---|---|
| Role | Reconnaissance aircraft |
| National origin | France |
| Manufacturer | SPAD |
| First flight | 17 January 1923 |
| Number built | 1 |
The Bleriot-SPAD S.36 was a French reconnaissance aircraft built in the early 1920s.
Design
The S.36 was a biplane with a monocoque fuselage of wood and canvas construction. Only one airframe was built, and flight tests ended due to the failure of the supercharger.
Specifications
Data from [1]
General characteristics
- Crew: 2
- Length: 9.02 m (29 ft 7 in)
- Wingspan: 11.46 m (37 ft 7 in)
- Height: 3.25 m (10 ft 8 in)
- Wing area: 39.00 m2 (419.8 sq ft)
- Empty weight: 1,017 kg (2,242 lb)
- Gross weight: 1,725 kg (3,803 lb)
- Powerplant: 1 × Hispano-Suiza 8F v-8 water-cooled piston engine, 220 kW (300 hp) with Rateau turbo-charger
- Propellers: 2-bladed fixed pitchpropeller
Performance
- Maximum speed: 200 km/h (120 mph, 110 kn)
See also
Related lists
References
- ↑ "SPAD S-36 - avion de reconnaissance - Un siècle d'aviation française". Aviafrance.com. https://www.aviafrance.com/spad-s-36-aviation-france-118.htm. Retrieved 2019-02-04.
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