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SPAD S.A

Pioneer and Early Aviation Aircraft

The SPAD S.A, also called the S.A.L., was a French two-seat tractor biplane that first flew in 1915 and was used by France and Russia in the early stages of the First World War as a fighter and reconnaissance aircraft. Its distinctive feature was a streamlined nacelle, called the pulpit, mounted ahead of the propeller to carry the observer and a machine gun, giving a clear field of fire at a time when synchronising gear was not yet available. Louis Béchereau designed it as the first aircraft built by SPAD after the company reorganised from Deperdussin, and it appeared in four main versions, the S.A-1 to S.A-4, built in small numbers, with about 42 delivered to France and 57 to the Imperial Russian Air Service. The pulpit vibrated badly and the arrangement was unpopular, but the experience led directly to the successful SPAD S.VII.

Facts
Year
1915 1
Engine Class
Rotary 1
Power (kW)
82 1
Top Speed (km/h)
140 1
Mass (kg)
414 1
Maximum Mass (kg)
674 1
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Exemplifies

Aviation, Modes
Source SPAD S.A (Wikipedia)

Of Make

Source SPAD S.A (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source SPAD S.A (Wikipedia)Design and development
Quote, Design and development
The SPAD A.1 prototype was the first aircraft produced by SPAD following its reorganization from the pre-war Deperdussin company.

Originated In

Also in Geography Atlas: where this subject originated.

Source SPAD S.A (Wikipedia)Lead
Quote, Lead
The SPAD S.A (also called S.A.L.) was a French two-seat tractor biplane first flown in 1915.
Sources
1. SPAD S.A (Wikipedia)
  • Lead
    The SPAD S.A (also called S.A.L.) was a French two-seat tractor biplane first flown in 1915.
  • Specifications (S.A-2)
    Powerplant: 1 × Le Rhône 9J 9-cylinder air-cooled rotary piston engine, 82 kW (110 hp)
  • Specifications (S.A-2), empty weight
    Empty weight: 414 kg (913 lb)
  • Specifications (S.A-2), gross weight
    Gross weight: 674 kg (1,486 lb)
  • Specifications (S.A-2), speed
    Maximum speed: 140 km/h (87 mph, 76 kn) at sea level
  • Design and development
    The SPAD A.1 prototype was the first aircraft produced by SPAD following its reorganization from the pre-war Deperdussin company.
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