Engineering:Blériot-SPAD S.31
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Revision as of 14:12, 17 March 2021 by imported>Scavis2 (url)
Short description: 1920s French aircraft
SPAD S.31 | |
---|---|
Role | Racer aircraft |
National origin | France |
Manufacturer | SPAD |
First flight | 1920 |
Number built | 1 |
The Bleriot-SPAD S.30 was a French racer aircraft built in the early 1920s.
Design
The S.31 was a biplane with a monocoque fuselage of wood and canvas construction, as well as floats. It was built to participate in the 1920 Schneider Cup.
Specifications
Data from [1]
General characteristics
- Crew: 1
- Length: 8.20 m (26 ft 11 in)
- Wingspan: 10.43 m (34 ft 3 in)
- Height: 3.42 m (11 ft 3 in)
- Wing area: 31.45 m2 (338.5 sq ft)
- Empty weight: 1,075 kg (2,370 lb)
- Gross weight: 1,510 kg (3,329 lb)
- Powerplant: 1 × Hispano-Suiza inline engine, 250 kW (340 hp)
- Propellers: 2-bladed fixed pitchpropeller
Performance
- Maximum speed: 210 km/h (130 mph, 110 kn)
See also
Related lists
References
- ↑ "SPAD S-31 - Hydravion de course - Un siècle d'aviation française". Aviafrance.com. 1997-05-05. https://www.aviafrance.com/spad-s-31-aviation-france-2554.htm. Retrieved 2019-02-04.
![]() | Original source: https://en.wikipedia.org/wiki/Blériot-SPAD S.31.
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