Hawker Danecock

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Danecock

One of the three original Danecocks
Type Fighter
Manufacturer Hawker Engineering Co.
Designed by Sydney Camm
Maiden flight 18 December 1925
Introduced 1925
Primary user Denmark
Produced 1925-1926
Number built 15
Developed from Hawker Woodcock

The Hawker Danecock biplane was developed from the Hawker Woodcock for the Danish air force and naval service.

Contents

[edit] Design and development

In 1925 the Danish Government notified Hawker that they would order three aircraft similar to the Woodcock, but with certain improvements. This resulted in Sydney Camm making minor changes to the wings and cockpit area. Compared to the Woodcock II, the Danecock had unequal span wings, a slightly lengthened fuselage, a 385 hp Armstrong Siddeley Jaguar IV engine and an armament of two 7.7 mm Madsen machine guns. The first aircraft was flown on 18 December 1925 by George Bulman with all three aircraft delivered in February 1926.

[edit] Operational history

After receiving the Hawker-built aircraft, Denmark obtained a licence to produce more Danecocks. This version, named the Dankok, was built in 1927 at the Danish Royal Naval Dockyard (Orlogsvaerftet). A total of 12 more were manufactured. One aircraft (a Hawker-build) broke the Scandinavian altitude record, reaching 28,208 ft (8,598 m). The Danecock/Dankok served until the mid-1930s when they were replaced by Hawker Nimrods. An example of the Dankok still exists in the Copenhagen Museum.

[edit] Operators

Flag of Denmark Denmark
  • Danish Army Air Service (Hærens Flyvertropper)
  • Danish Naval Air Service (Marinens Flyvevæsen)

[edit] Specifications

Data from Hawker Aircraft since 1920[1]

General characteristics

  • Crew: one, pilot
  • Length: 26 ft 1¼ in (7.95 m)
  • Wingspan: 32 ft 7 in (9.93 m)
  • Height: 10 ft 1 in (3.05 m)
  • Wing area: 340 ft² (31.59 m²)
  • Empty weight: 2,128 lb (965.2 kg)
  • Loaded weight: 3,045 lb (1,381.2 kg)
  • Powerplant: 1× Armstrong Siddeley Jaguar IV 14-cylinder air-cooled double radial engine, 385 hp (287 kW)

Performance

Armament

[edit] See also

Related lists

[edit] References

  1. ^ Mason, Francis K. Hawker Aircraft since 1920. London: Putnam & Co., 1961. ISBN 1-85310-270-9.
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