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Caudron Typhon

From Wikipedia, the free encyclopedia

Caudron Typhon
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The Caudron C.640 Typhon was a 1930s French high-speed single-seat monoplane utility aircraft built by Caudron-Renault.

Quick Facts Typhon, General information ...
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History

Similar in concept to the de Havilland DH.88 Comet the Typhon (en: Typhoon) was designed by Georges Otfinovsky and Marcel Riffard for use on long-range postal routes.[1] The first aircraft first flew on 17 June 1935.[2] The aircraft was a twin-engined low-wing cantilever monoplane of wooden construction. Seven C.640s were built. The Typhon established 5000 km speed records. It was not a success in operation as its flexible wings experienced buffeting and vibration problems.

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Variants

  • C.640 Typhon - production model with Renault 6Q engines, 7 built.
  • C.641 Typhon - record breaking version with raised canopy and increased fuel capacity, 2 built.
  • C.670 Typhon - prototype high-speed bomber version with a crew of three, similar to the C.640 but with increased dimensions and weights, one built.

Operators

France
Romania

Specifications (C.640)

Data from Aviafrance : Caudron C.640 'Typhon'[3]

General characteristics

  • Crew: 2
  • Length: 10.95 m (35 ft 11 in)
  • Wingspan: 11.5 m (37 ft 9 in)
  • Height: 3 m (9 ft 10 in)
  • Wing area: 28 m2 (300 sq ft)
  • Empty weight: 1,630 kg (3,594 lb)
  • Gross weight: 3,400 kg (7,496 lb)
  • Powerplant: 2 × Renault 6Q 6-cylinder inverted air-cooled in-line piston engines, 164 kW (220 hp) each
  • Propellers: 2-bladed Ratier

Performance

  • Maximum speed: 400 km/h (250 mph, 220 kn)
  • Cruise speed: 370 km/h (230 mph, 200 kn)
  • Range: 3,725 km (2,315 mi, 2,011 nmi)
  • Service ceiling: 7,000 m (23,000 ft)
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See also

Aircraft of comparable role, configuration, and era

References

Further reading

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