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Blériot-SPAD S.41

From Wikipedia, the free encyclopedia

S.41
Role Fighter
Manufacturer Blériot
Designer André Herbemont
First flight 16 July 1922
Primary user Aéronautique Militaire
Number built 1

The Blériot-SPAD S.41 was a French fighter aircraft developed in the early 1920s.

Design and development

The S.41 was a refinement of the S.XX and was a single-seat fighter biplane which had a monocoque fuselage made of wood. The wings, on the other hand, were made of wood and metal.[1] In 1924, the S.41 was converted to a racer and redesignated S.41bis.

Specifications

Data from [2]

General characteristics

  • Crew: one
  • Length: 6.65 m (21 ft 10 in)
  • Wingspan: 8.68 m (28 ft 6 in)
  • Height: 2.76 m (9 ft 1 in)
  • Wing area: 26.40 m2 (284.2 sq ft)
  • Empty weight: 887 kg (1,956 lb)
  • Gross weight: 1,307 kg (2,881 lb)
  • Powerplant: 1 × Hispano-Suiza 8Fb inline engine , 224 kW (300 hp)

Performance

  • Maximum speed: 238 km/h (148 mph, 129 kn)
  • Cruise speed: 205 km/h (127 mph, 111 kn)
  • Service ceiling: 6,850 m (22,470 ft)

Armament

See also

Related development

References

  1. ^ "SPAD S-41 - avion de chasse - Un siècle d'aviation française". Aviafrance.com. Retrieved 2019-02-03.
  2. ^ "SPAD S.41". www.airwar.ru.

Bibliography

  • Bruner, Georges (1977). "Fighters a la Francaise, Part One". Air Enthusiast (3): 85–95. ISSN 0143-5450.
This page was last edited on 24 January 2022, at 09:22
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