The Blériot-SPAD S.38 was a French fighter aircraft developed in the early 1920s. It was a single-seat fighter of all-wood construction with canvas covering, and the aircraft was intended to test a cable hook. The specification lists a crew of one, a length of 5.51 m, a wingspan of 7.1 m, a height of 4 m, a wing area of 16 square metres, an empty weight of 380 kg and a gross weight of 500 kg, with one 60 kW Le Rhône 9C nine-cylinder air-cooled rotary piston engine. The English Wikipedia article states no speed for it.
Facts
Engine Class Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.38 (Wikipedia)
Of Make
Source Blériot-SPAD S.38 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.38 (Wikipedia)LeadQuote, Lead
The Blériot-SPAD S.38 was a French fighter aircraft developed in the early 1920s.
Originated In
Also in Geography Atlas: where this subject originated.
Source Blériot-SPAD S.38 (Wikipedia)LeadQuote, Lead
The Blériot-SPAD S.38 was a French fighter aircraft developed in the early 1920s.
Sources
1. Blériot-SPAD S.38 (Wikipedia)
Specifications
Empty weight: 380 kg (838 lb)
Specifications, maximum mass
Gross weight: 500 kg (1,102 lb)
Specifications, powerplant
Le Rhône 9C 9-cylinder air-cooled rotary piston engine, 60 kW (80 hp)
Lead
The Blériot-SPAD S.38 was a French fighter aircraft developed in the early 1920s.
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