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Blériot-SPAD S.31

Pioneer and Early Aviation Aircraft

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
Power (kW)
250 1
Top Speed (km/h)
210 1
Mass (kg)
1075 1
Maximum Mass (kg)
1510 1
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Exemplifies

Aviation, Modes
Source Blériot-SPAD S.31 (Wikipedia)

Of Make

Source Blériot-SPAD S.31 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Blériot-SPAD S.31 (Wikipedia)Lead, manufacturer
Quote, 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)Lead
Quote, 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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