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Blériot-SPAD S.25

Pioneer and Early Aviation Aircraft

The Blériot-SPAD S.25 was a single-seat long-distance aeroplane built at the request of Leith Jensen, who wanted to fly from Newfoundland to Iceland. It was a biplane with a monocoque fuselage of wood and canvas construction, designed with a watertight fuselage and with quick-emptying tanks that could serve as floats where appropriate. Jensen's attempt was abandoned after the feat of Alcock and Brown, so the S.25 flew on 29 August 1921 as a sports aircraft instead. The specification lists a crew of one, a length of 6.50 m, a wingspan of 8.12 m, an empty weight of 467 kg, a gross weight of 931 kg and a maximum speed of 160 km/h from one 71 kW Le Rhône nine-cylinder rotary piston engine.

Facts
Year
1921 1
Engine Class
Piston 1
Power (kW)
71 1
Top Speed (km/h)
160 1
Mass (kg)
467 1
Maximum Mass (kg)
931 1
Connections

Exemplifies

Aviation, Modes
Source Blériot-SPAD S.25 (Wikipedia)

Of Make

Source Blériot-SPAD S.25 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Blériot-SPAD S.25 (Wikipedia)Lead
Quote, Lead
The Bleriot-SPAD S.25 was a single-seater long-distance airplane built at the request of Leith Jensen who wanted to connect Newfoundland to Iceland.
Sources
1. Blériot-SPAD S.25 (Wikipedia)
  • Design
    so the S.25 flew on August 29, 1921 as a sports aircraft
  • Specifications
    Empty weight: 467 kg (1,030 lb)
  • Specifications, maximum mass
    Gross weight: 931 kg (2,053 lb)
  • Specifications, top speed
    Maximum speed: 160 km/h (99 mph, 86 kn)
  • Specifications, powerplant
    Le Rhone 9-cylinder rotary piston engine, 71 kW (95 hp)
  • Lead
    The Bleriot-SPAD S.25 was a single-seater long-distance airplane built at the request of Leith Jensen who wanted to connect Newfoundland to Iceland.
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