The Blériot-SPAD S.31 was a French racer aircraft built in the early 1920s. It was a biplane with a monocoque fuselage of wood and canvas construction, fitted with floats, and it was built to take part in the 1920 Schneider Cup. The specification lists a crew of one, a length of 8.20 m, a wingspan of 10.43 m, a height of 3.42 m, a wing area of 31.45 square metres, an empty weight of 1,075 kg, a gross weight of 1,510 kg and a maximum speed of 210 km/h from one 250 kW Hispano-Suiza inline engine. The lead sentence of the English Wikipedia article gives the type as the S.30, which its own design section and title correct to S.31.
Facts
Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.31 (Wikipedia)
Of Make
Source Blériot-SPAD S.31 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.31 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
The Bleriot-SPAD S.30 was a French racer aircraft built in the early 1920s.
Originated In
Also in Geography Atlas: where this subject originated.
Source Blériot-SPAD S.31 (Wikipedia)LeadQuote, Lead
was a French racer aircraft built in the early 1920s.
Sources
1. Blériot-SPAD S.31 (Wikipedia)
Specifications
Empty weight: 1,075 kg (2,370 lb)
Specifications, maximum mass
Gross weight: 1,510 kg (3,329 lb)
Specifications, top speed
Maximum speed: 210 km/h (130 mph, 110 kn)
Specifications, powerplant
Hispano-Suiza inline engine, 250 kW (340 hp)
Lead
was a French racer aircraft built in the early 1920s.
Lead, manufacturer
The Bleriot-SPAD S.30 was a French racer aircraft built in the early 1920s.
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