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
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.25 (Wikipedia)
Of Make
Source Blériot-SPAD S.25 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.25 (Wikipedia)LeadQuote, 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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