The Blériot-SPAD S.36 was a French reconnaissance aircraft built in the early 1920s. It was a biplane with a monocoque fuselage of wood and canvas construction. Only one airframe was built, and flight tests ended because the supercharger failed. The specification lists a crew of two, a length of 9.02 m, a wingspan of 11.46 m, a height of 3.25 m, a wing area of 39 square metres, an empty weight of 1,017 kg, a gross weight of 1,725 kg and a maximum speed of 200 km/h from one 220 kW Hispano-Suiza 8F water-cooled V-8 piston engine fitted with a Rateau turbocharger.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.36 (Wikipedia)
Of Make
Source Blériot-SPAD S.36 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.36 (Wikipedia)LeadQuote, Lead
The Bleriot-SPAD S.36 was a French reconnaissance aircraft built in the early 1920s.
Originated In
Also in Geography Atlas: where this subject originated.
Source Blériot-SPAD S.36 (Wikipedia)LeadQuote, Lead
The Bleriot-SPAD S.36 was a French reconnaissance aircraft built in the early 1920s.
Sources
1. Blériot-SPAD S.36 (Wikipedia)
Specifications
Empty weight: 1,017 kg (2,242 lb)
Specifications, maximum mass
Gross weight: 1,725 kg (3,803 lb)
Specifications, top speed
Maximum speed: 200 km/h (120 mph, 110 kn)
Specifications, powerplant
Hispano-Suiza 8F v-8 water-cooled piston engine, 220 kW (300 hp)
Design
Only one airframe was built
Lead
The Bleriot-SPAD S.36 was a French reconnaissance aircraft built in the early 1920s.
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