To meet the requirements of Air Ministry Specification F.20/27, Sydney Camm of Hawker designed a single seat fighter biplane, which flew for the first time in August 1928 powered by a 450 hp Bristol Jupiter VII radial engine. It was also tested with a 520 hp Bristol Mercury VI powerplant, also a radial, and the satisfactory results inspired the design of the Hornet prototype. It was clear to Sydney Camm at Hawkers that the F.20/27 specification would soon have to be revised, and so in 1929 Hawkers began work on the Hornet. which utilized the 420 hp (313 kW) Rolls Royce F.XIA V type engine enclosed by a smooth, streamlined cowling.

The new fighter prototype was a single engined biplane, with single bay wings, known as the Hawker Hornet, first flew at Brooklands, Surrey, in March 1929. It used Hawker’s tubular steel construction method and all metal structure.

The Hornet made its public debut at the 1929 Olympia Aero Show. The engine was changed for a 480 hp (358 kW) F.XIS when it was sent for service trials. Registered J9682, the Hornet was purchased by the Air Ministry in September 1929 and renamed Fury I, and delivered to Martlesham Heath for service trials. It was evaluated against the similarly powered Fairey Firefly II, being preferred because of its better handling compared with the mainly wooden construction of the Firefly.

The private venture prototype (G ABSE) made its first flight on April 13, 1932, and was developed as the Intermediate Fury. From this was evolved the High Speed Fury, also a private venture, flown for the first time on May 3, 1933, and subsequently fitted with various Rolls Royce Kestrel or Goshawk engines. British Aerospace records suggest that this biplane was re-engined in 1934 with a Goshawk III and flown on 17 October of that year, with which it attained a speed of 394km/h, subsequently receiving a later 518kW Goshawk engine. After evaluation, Specification 6/35 was issued to cover the production of 23 similar aircraft ordered initially in August 1930, with 640 hp Kestrel VI engines, as Fury IIs for the RAF.

Officially, the Fury was constructed under Specification 13/30, though it would be more accurate to say that the specification was written round the Fury. The fighter had a standard tubular metal airframe of rectangular section, fairing into an oval; the forward fuselage was metal skinned and the rear portion fabric covered. The staggered, unequal span wings had ailerons on the upper mainplane only, and the wooden two blade prop¬eller was driven by a supercharged 525 hp Rolls Royce Kestrel IIS engine, the developed version of the F.Xl. Standard armament comprised two synchronized Vickers 0.303 in (7.7 mm) machine guns in the nose and racks for light bombs could be fitted beneath the lower wings.

The first production Fury I flew on March 25, 1931. No 43 Squadron received 16 aircraft in May 1931, and Nos 1 and 25 Squadrons were equipped from orders placed during that year. The Fury had an exceptionally rapid rate of climb, 3048 m (10 000 ft) in 41 minutes, was highly manoeuvrable, and was the first intercepter with the RAF capable of achiev¬ing a level speed of more than 322 kph (200 mph).

General Aircraft was given an order for 75 of this version, but this was not completely fulfilled though it included a few Fury IIs for South Africa.

In 1934 it was decided that a Fury I should be fitted with a Kestrel VI with composite cooling, modified fuel and oil systems and streamlined wheel spats as the Fury II. This was first flown on 20 August 1935. Twenty-three production Fury IIs were built by Hawker with increased fuel capacity, followed by 89 from General Aircraft, six of which were delivered to the South African Air Force.

Fury IIs entered RAF service (with No 25 Squadron) in early 1937, but the five squadrons equipped with the Mk II had begun phasing them out by January 1939. However, 16 Fury Is and.48 Fury IIs were still serving, with RAF training units, at the beginning of the Second World War.

Altogether 118 were completed for the RAF with 391kW Kestrel IIS engines.

Hawker Fury number 401 was exported to Norway for evaluation. It was powered by the Armstrong Siddeley Panther IIIA radial engine, and made its first flight on September 9 of the same year. The aircraft was tested briefly at Brooklands and Martiesham and then flown to Oslo by P. W. S. Bulman. It was later tested with a ski undercarriage, but plans to produce the type in Norway did not materialise due to c.g. problems.

Six Pratt & Whitney Hornet-powered Furies went to Persia, three Furies to Portugal, and six Hispano-Suiza 12-engined aircraft to Yugoslavia.

Spanish Fury I Article

These foreign models were armed with various calibre machine guns of Colt, Mauser or Spandau manufacture, and those supplied to Yugoslavia could carry two additional machine guns beneath the lower wings.

Gallery

Hawker Hornet
Engine: Rolls-Royce F.XIS. 480hp
Wing span: 30ft 0in
Length: 26ft 3in
Height: 9ft 4in
Empty Weight: 2,409lb
Loaded Weight: 3,232lb
Max Speed: 205mph at 13,000ft
Climb: 5min 9sec to 10,000ft
Service Ceiling: 25,500ft
Armament: Provision for two Vickers Mk III guns
Crew: 1

Fury I
Engine: One 525 hp Rolls Royce Kestrel IIS.
Span: 9.14 m (30 ft)
Length: 8.13 m (26 ft 8 in)
Weight empty 2,623 lb. (1,190 kg.)
Gross weight: 1583 kg (3490 lb)
Maximum speed: 333 km/h (207 mph).
Ceiling 28,000 ft. (8,500 m.) fully loaded.
Range 305 miles (490 km.)
Crew: 1.
Armament: Two synchronised machine¬ guns.

Fury Mk II
Engine: 1 x Rolls-Royce Kestrel VI, 477kW / 631 hp
Max take-off weight: 1637 kg / 3609 lb
Empty weight: 1240 kg / 2734 lb
Wingspan: 9.14 m / 29 ft 12 in
Length: 8.15 m / 26 ft 9 in
Height: 3.10 m / 10 ft 2 in
Wing area: 23.41 sq.m / 251.98 sq ft
Wing loading: 14.35 lb/sq.ft / 70.0 kg/sq.m
Max. speed: 194 kts / 359 km/h / 223 mph
Service ceiling: 8990 m / 29500 ft
Range: 235 nm / 435 km / 270 miles
Armament: 2x cal.303 MG (7,7mm)
Crew: 1

The Hind light bomber was one of the types produced for quick delivery to the RAF, based on the Hart and therefore needing little new development, although a number of improvements were introduced as the result of long experience with the Hart.

The first prototype was a modified Hart and first flew on 12 September 1934 at Brooklands.

Hawker Hind Article

By the end of 1935 the Hind had started to replace the Hawker Hart as a front line fighter with the RAF.
The production total was 528 aircraft, although with the delivery of modern monoplane bombers a number of the final Hinds on the production lines for the RAF were completed as dual-control trainers. Records show that from even the first batch of 20 Hinds, General Aircraft was later to convert nine into trainers.

Nine foreign users of the Hind (new and ex-RAF aircraft) included Latvia, New Zealand, Persia and South Africa.

Engine: 1 x Rolls-Royce Kestrel V, 477kW / 631 hp
Max take-off weight: 2403 kg / 5298 lb
Empty weight: 1475 kg / 3252 lb
Wingspan: 11.35 m / 37 ft 3 in
Length: 9.02 m / 29 ft 7 in
Height: 3.23 m / 10 ft 7 in
Wing area: 32.33 sq.m / 348.00 sq ft
Max. speed: 161 kts / 299 km/h / 186 mph @ 16,000 ft
Service ceiling: 8045 m / 26400 ft
Initial climb rate: 1870.08 ft/min / 9.50 m/s
Range: 374 nm / 692 km / 430 miles
Armament: 2 x 7.7mm machine-guns, 220kg of bombs
Crew: 2
Endurance: 4 h

The Osprey was a two-seat naval fighter-reconnaissance biplane, developed from the Hart but with additional strengthening for catapult launching, folding wings for storage on board ship and naval equipment.

The first prototype flew in 1930 and was eventually followed by 37 Osprey Mk I, 14 Mk II, 52 Mk III and 26 Mk IV production aircraft; the Mk IIs later being modified into Mk IIIs with Fairey Reid propellers and other refinements.
A small number of the genuine Mk IIIs were constructed of stainless steel, one of which, according to Hawker records, was exhibited in skeleton form at the 1932 Paris Show.
Standard power plant for the Mk Is, IIs and IIIs was the 423kW Rolls-Royce Kestrel IIMS, giving a maximum speed of 257km/h as a landplane.
Seaplane Ospreys had twin floats, although an experiment was carried out with one aircraft fitted with a central main float and wingtip stabilising floats.
The Mk IV was powered by a 477kW Kestrel V engine.

Ospreys entered service with the FAA in 1932 and eventually flew from aircraft carriers, cruisers and other warships. In 1934 one RAF squadron took delivery of four Ospreys for communications work, and in the same year HMS Sussex went to Melbourne as part of the Centenary celebrations carrying an Osprey. By mid-1935 several ships of the Second Cruiser Squadron of the Home Fleet had been issued with Ospreys and the new cruiser Ajax had received two for service with the Mediterranean Command. These remained in service until 1939.
The Swedish vessel Gotland had received Mercury-powered Ospreys, known as Nohabs. These remained operational as naval co-operation aircraft alongside Heinkel He 5s until 1940.
Three Ospreys were also delivered to Portugal and Spain, although it is uncertain whether the Spanish aircraft was among the 57 machines sent by Britain to the Republican Air Force during the Civil War.

Osprey Mk III
Engine: 423kW Rolls-Royce Kestrel IIMS
Max take-off weight: 2245 kg / 4949 lb
Empty weight: 1545 kg / 3406 lb
Wingspan: 11.28 m / 37 ft 0 in
Length: 8.94 m / 29 ft 4 in
Height: 3.17 m / 10 ft 5 in
Wing area: 31.5 sq.m / 339.06 sq ft
Max. speed: 270 km/h / 168 mph
Ceiling: 7165 m / 23500 ft

Osprey Mk IV
Engine: Rolls Royce Kestrel V, 631 hp
Length: 29.331 ft / 8.94 m
Height: 10.4 ft / 3.17 m
Wingspan: 37.008 ft / 11.28 m
Wing area: 338.958 sq.ft / 31.49 sq.m
Max take off weight: 4950.2 lb / 2245.0 kg
Weight empty: 3404.5 lb / 1544.0 kg
Max. speed: 153 kts / 283 km/h
Cruising speed: 94 kts / 175 km/h
Service ceiling: 25000 ft / 7620 m
Wing loading: 14.56 lb/sq.ft / 71.0 kg/sq.m
Endurance: 2 h
Crew: 2
Armament: 2x cal.303 MG (7,7mm)

The Hawker Hartebeeste (also known as Hartbee or Hartebees) was a version of the Hawker Audax air co-operation aircraft modified for use in South Africa. The first was flown on 1 June 1928, and four (s/n 801 to 804) were produced by Hawker in 1934-35, with another sixty five (s/n 805 to 869) built by Roberts Heights in Pretoria, South Africa from 1937. The main difference between the Hartebeeste and the Audax was a change of engine to the Rolls Royce Kestrel VFP, producing 608hp. The more powerful engine compensated for the addition of some armour around the cockpits.

The Hartebeeste had a short front line career with the South African Air Force. Introduced on 1 January, 1930, two squadrons were equipped with the Hartebeeste when the Italians entered the war on 10 June 1940. The next day the Hartebeeste’s undertook their biggest operation of the war, a large scale attack on Italian positions. Soon after that the Hartebeeste was withdrawn from the front line, and transferred to training and communications units, remaining in service for the rest of the war.

Hawker Hartebeeste
Engine: Rolls Royce Kestrel V FP, 600 hp / 453kW
Total Length: 29ft 7in / 9.020 m
Greatest height: 10 ft 5 in / 3.170 m
Wingspan: 37ft 3in / 11.350 m
Wing area: 348.000 sqft / 32.330 sq.m
Max take off weight: 4787.1 lbs / 2171.0 kg
Weight empty: 3150 lbs / 1429.0 kg
Max. speed: 153 kts / 283 km/h / 176 mph
Service ceiling: 22,000 ft / 6705 m
Wing load: 13.74 lbs/sq.ft / 67.00 kg/qm
Endurance: 3 h
Crew: 2
Armament: 2 x .303 MG (7,7mm), one forward firing and one in aft cockpit plus light bombs or supply canisters under the wings.