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Blériot-SPAD S.26

The Bleriot-SPAD S.26 was a seaplane racer aircraft built in the late 1910s.

SPAD S.26
Role Seaplane racer
National origin France
Manufacturer SPAD
First flight 28 August 1919
Number built 1

Design edit

The S.26 was a biplane with a monocoque fuselage of wood and canvas construction as well as floats. Although intended to take part in the 1919 Schneider Cup, a puncture in one of the floats during flight testing eliminated it from the Schneider Cup.

Specifications edit

Data from [1]

General characteristics

  • Crew: 1
  • Length: 8.10 m (26 ft 7 in)
  • Wingspan: 8.69 m (28 ft 6 in)
  • Height: 3.16 m (10 ft 4 in)
  • Wing area: 26 m2 (280 sq ft)
  • Empty weight: 850 kg (1,874 lb)
  • Gross weight: 1,130 kg (2,491 lb)
  • Powerplant: 1 × Hispano-Suiza inline engine, 250 kW (340 hp)
  • Propellers: 2-bladed fixed pitchpropeller

Performance

  • Maximum speed: 250 km/h (160 mph, 130 kn)

See also edit

Related lists

References edit

  1. ^ "SPAD S-26 - Hydravion de course - Un siècle d'aviation française". Aviafrance.com. 1999-01-26. Retrieved 2022-08-31.

blériot, spad, bleriot, spad, seaplane, racer, aircraft, built, late, 1910s, spad, 26role, seaplane, racernational, origin, francemanufacturer, spadfirst, flight, august, 1919number, built, 1design, editthe, biplane, with, monocoque, fuselage, wood, canvas, co. The Bleriot SPAD S 26 was a seaplane racer aircraft built in the late 1910s SPAD S 26Role Seaplane racerNational origin FranceManufacturer SPADFirst flight 28 August 1919Number built 1Design editThe S 26 was a biplane with a monocoque fuselage of wood and canvas construction as well as floats Although intended to take part in the 1919 Schneider Cup a puncture in one of the floats during flight testing eliminated it from the Schneider Cup Specifications editData from 1 General characteristicsCrew 1 Length 8 10 m 26 ft 7 in Wingspan 8 69 m 28 ft 6 in Height 3 16 m 10 ft 4 in Wing area 26 m2 280 sq ft Empty weight 850 kg 1 874 lb Gross weight 1 130 kg 2 491 lb Powerplant 1 Hispano Suiza inline engine 250 kW 340 hp Propellers 2 bladed fixed pitchpropellerPerformance Maximum speed 250 km h 160 mph 130 kn See also editRelated lists List of Interwar military aircraftReferences edit SPAD S 26 Hydravion de course Un siecle d aviation francaise Aviafrance com 1999 01 26 Retrieved 2022 08 31 Retrieved from https en wikipedia org w index php title Bleriot SPAD S 26 amp oldid 1157325832, wikipedia, wiki, book, books, library,

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