Hawker Woodcock

Hawker Woodcock

Hawker Woodcocks from No. 3 Squadron
Role	Fighter
National origin	United Kingdom
Manufacturer	Hawker
Designer	Capt. Thomson W.G. Carter
First flight	March 1923
Introduction	1924
Primary user	Royal Air Force
Produced	1924-1926
Number built	64
Variants	Hawker Danecock

The Hawker Woodcock was a British single-seat fighter built by the Hawker Engineering Company as the first fighter to be produced by Hawker Engineering (the successor to Sopwith Aviation). It was used by the RAF as a night fighter in the 1920s.

Design and development

The Hawker Woodcock was designed as a night fighter in 1922 to meet specification 25/22.^[1] The chief designer was Captain Thomson, and the prototype, serial number J6987, was first flown with a 358 hp (267 kW) Armstrong Siddeley Jaguar II engine in March 1923 with F. P. Raynham at the controls. It featured a two-bay wing with the inner struts at about ⅓ span.

The prototype was rejected because of lack of manoeuvrability as well as suffering from serious wing flutter and ineffective rudder control. Following the first flight W. G. Carter took over as chief designer and changed the design, reducing the wingspan by 2 ft (0.61 m) and making it a single-bay structure. The powerplant was changed to a 380 hp (283 kW) Bristol Jupiter IV engine. The modified design was designated the Woodcock Mk II and first flew in July 1923. A number of accidents occurred and the design was progressively strengthened until the structural weakness had been cured.

The Woodcock was armed with two .303 in (7.7 mm) Vickers machine guns, synchronised to fire through the propeller arc. The guns were mounted externally on each side of the fuselage, just below the edge of the cockpit.

The first order for the Royal Air Force was for ten Woodcock IIs, with the first six being completed without any night flying equipment.^[1] The service eventually ordered a total of 62 aircraft. One of the first batch of aircraft was given a civil registration to allow it to be demonstrated in Scandinavia.^[1]^[2] On return to the United Kingdom, the demonstrator was entered into the 1925 King's Cup Air Race but it crashed during the race in bad weather near Luton.^[1]

Operational history

The first aircraft to be delivered to the Royal Air Force entered service with 3 Squadron in May 1925 at RAF Upavon. No. 17 Squadron was the only other operational squadron, with first deliveries being made in March 1926. Once the type's early structural problems were solved, the Woodcock proved popular with its pilots. It was replaced by the Gloster Gamecock in 1928. However, some Woodcocks were still flying in 1936.^[3]

In June 1927 a Woodcock II of No. 17 Squadron was borrowed by the notable aviator Charles Lindbergh.^[1] He used the aircraft to fly back to Paris from London soon after his transatlantic flight in the Spirit of St. Louis.^[1]

Hawker Woodcock Mk II

Variants

Woodcock Mk I: Single-seat night fighter prototype with two-bay equal-span wings and a 358hp Armstrong Siddeley Jaguar II engine, one built.^[1]
Woodcock Mk II: Single-seat night fighter for the RAF with a Bristol Jupiter IV engine and other design changes, One prototype and 62 production aircraft built.^[1]
Hawker Danecock: Single-seat fighter aircraft for Denmark with Jaguar IV engines and Madsen machine guns. Three aircraft were built.^[1]
L.B II Dankok: Single-seat fighter aircraft for the Danish Army Air Service, and the Danish Naval Air Service. A total of 12 were built under licence in Denmark.

Operators

United Kingdom

Royal Air Force
- No. 3 Squadron RAF
- No. 17 Squadron RAF

Denmark

Danish Army Air Service and Danish Naval Air Service: 12 license-built L.B II Dankok.

Specifications (Woodcock Mk II)

Data from The British Fighter since 1912^[4]

General characteristics

Crew: one
Length: 25 ft 7 in (7.80 m)
Wingspan: 34 ft 8 in (10.57 m)
Height: 9 ft (2.74 m)
Wing area: 356 ft² (33.1 m²)
Empty weight: 2,014 lb (915 kg)
Loaded weight: 2,979 lb (1,354 kg)
Powerplant: 1 × Bristol Jupiter IV 9-cylinder radial engine, 425 hp (317 kW)

Performance

Maximum speed: 123 kn (141 mph, 227 km/h)
Cruise speed: 90 kn (103 mph,^[5] 166 km/h)
Range: 243 nmi (280 mi, 451 km)
Service ceiling: 20,550 ft (6,270 m)
Wing loading: 8.37 lb/ft² (40.9 kg/m²)
Power/mass: 0.143 hp/lb (0.234 kW/kg)
Climb to 10,000 ft (3,050 m): 8 min 20 sec

Armament

2 × .303 in (7.7 mm) Vickers machine guns on sides of fuselage

References

Notes

1 2 3 4 5 6 7 8 9 Munson, Kenneth. 'Woodcock and Fury - Hawker's first and last biplane fighters." Aircraft Illustrated Extra, Issue 4, May 1970, Ian Allan Limited, pp. 6–12.
↑ "Registration G-EBMA." United Kingdom Civil Aviation Authority. Retrieved: 2 November 2009.
↑ Mason 1991, p. 106.
↑ Mason 1992, p. 169.
↑ Jackson 1973, p. 345.

Bibliography

Jackson, A.J. British Civil Aircraft since 1919, Volume 1, 2nd Edition. London: Putnam, 1973. ISBN 0-370-10006-9.
Mason, Francis K. The British Fighter since 1912. Annapolis, Maryland: Naval Institute Press, 1992. ISBN 1-55750-082-7.
Mason, Francis K. Hawker Aircraft since 1920. London: Putnam, 1991. ISBN 0-85177-839-9.

External links

Wikimedia Commons has media related to Hawker Woodcock.

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