Cierva C.24

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C.24
Cierva C.24 (G-ABLM).jpg
de Havilland C.24 in flight
RoleUtility autogyro
Manufacturer de Havilland
Designer Juan de la Cierva
First flight September 1931 [1]
StatusMuseum exhibit
Produced1931
Number built1

The de Havilland C.24 was a two-seat autogyro built by de Havilland at its Stag Lane works in England in 1931

Contents

Design and development

The C.24 was built in 1931 using a Cierva rotor head coupled to the cabin of a de Havilland DH.80A Puss Moth, and driven by a 120 hp Gipsy III engine. It was withdrawn from use by December 1934. [2]

A single example (G-ABLM) was produced and is part of the Science Museum collection. In 1932, it was redesignated C.26 (not to be confused with the unbuilt C.26 twin-engine autogiro design) when a two-blade rotor system was installed. [3] Since 2008 it has been on loan to the de Havilland Aircraft Museum at Salisbury Hall, near London Colney in Hertfordshire. In flight, it had a maximum speed of about 115 mph (185 km/h; 100 kn).

Specifications

Data from Jackson 1978 p.524 [1]

General characteristics

Performance

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References

Citations

  1. 1 2 Jackson 1978, pp. 524
  2. "UK Certificate of Registration No. 3138, 22 April 1931" (PDF). UK Civil Aviation Authority. Archived from the original (PDF) on 6 June 2011. Retrieved 11 January 2009.
  3. "De Havilland - Cierva C.24 - Stingray's List of Rotorcraft".

Bibliography

  • Jackson, A.J. (1978). de Havilland Aircraft since 1909. London: Putnam Publishing. ISBN   0-370-30022-X.