The Blériot-SPAD S.30 was a French sports aircraft built in the early 1920s. It was a biplane with a monocoque fuselage of wood and canvas construction, and it was the first French aircraft to be built and equipped with a NACA cover. In September 1920, after initial flight tests, it was re-engined with a Le Rhône engine and redesignated S.30bis. The specification lists a crew of one, a length of 5.94 m, a wingspan of 7.14 m, a height of 2.24 m and a wing area of 15.40 square metres, with an empty weight of 333 kg, a gross weight of 460 kg and a maximum speed of 170 km/h from a 34 kW Anzani inline engine.
Facts
Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.30 (Wikipedia)
Of Make
Source Blériot-SPAD S.30 (Wikipedia)
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Manufactured By
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Source Blériot-SPAD S.30 (Wikipedia)LeadQuote, Lead
The Bleriot-SPAD S.30 was a French sports aircraft built in the early 1920s.
Originated In
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Source Blériot-SPAD S.30 (Wikipedia)LeadQuote, Lead
The Bleriot-SPAD S.30 was a French sports aircraft built in the early 1920s.
Sources
1. Wikipedia: Bleriot
Aircraft, Blériot-SPAD aircraftQuote, Aircraft, Blériot-SPAD aircraft
Blériot-SPAD S.30 (1920) Single-seat sport aircraft.
2. Blériot-SPAD S.30 (Wikipedia)
Specifications
Empty weight: 333 kg (734 lb)
Specifications, maximum mass
Gross weight: 460 kg (1,014 lb)
Specifications, top speed
Maximum speed: 170 km/h (110 mph, 92 kn)
Specifications, powerplant
Anzani inline engine, 34 kW (45 hp)
Lead
The Bleriot-SPAD S.30 was a French sports aircraft built in the early 1920s.
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