The Blériot-SPAD S.39 was a French carrier-borne reconnaissance aircraft built in the early 1920s. It was a biplane with a monocoque fuselage and wings of wood and canvas, and its undercarriage featured a hydroplane or flotation device. The specification lists a crew of two, a length of 7.83 m, a wingspan of 10.43 m, a height of 2.93 m, a wing area of 33 square metres, an empty weight of 1,028 kg, a gross weight of 1,520 kg and a maximum speed of 220 km/h from one 205 kW Hispano-Suiza engine driving a two-bladed fixed-pitch propeller. The article does not say what type of engine it was.
Facts
Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.39 (Wikipedia)
Of Make
Source Blériot-SPAD S.39 (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.39 (Wikipedia)LeadQuote, Lead
The Bleriot-SPAD S.39 was a French carrier-borne reconnaissance aircraft built in the early 1920s.
Originated In
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Source Blériot-SPAD S.39 (Wikipedia)LeadQuote, Lead
The Bleriot-SPAD S.39 was a French carrier-borne reconnaissance aircraft built in the early 1920s.
Sources
1. Blériot-SPAD S.39 (Wikipedia)
Specifications
Empty weight: 1,028 kg (2,266 lb)
Specifications, maximum mass
Gross weight: 1,520 kg (3,351 lb)
Specifications, top speed
Maximum speed: 220 km/h (140 mph, 120 kn)
Specifications, powerplant
205 kW (275 hp)
Lead
The Bleriot-SPAD S.39 was a French carrier-borne reconnaissance aircraft built in the early 1920s.
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