Hawker Tornado

Sydney Camm and his team responded to Specification F.18/37 that called for a single-seat interceptor, with two tenders. One was referred to as the “R-type” and the other as the “N-type”. These were to use fundamentally similar airframes and differ essentially in the type of engine installed. The “R-type”, which was to be named Tornado, initially appeared the most promising and was powered by a 24-cylinder X-type Rolls-Royce Vulture – basically two 12-cylinder Peregrine V engines driving a common crankshaft.
The first of two prototypes was flown on 6 October 1939 with a 1760hp Vulture II, provision being made for an armament of 12 7.7mm machine guns. The similarly-powered second prototype, flown on 5 December 1940, had provision for a four 20mm cannon armament.
In May 1940, the war situation led to the cancellation of all priority for Typhoon and Tornado development in order to allow every effort to be put into the production of sorely needed Hurricanes. Design development was allowed to continue, however, and during 1940 three alternative engine installations were proposed for the Tornado–the Fairey Monarch, the Wright Duplex Cyclone, and the Bristol Centaurus – and experimental drawings for the Centaurus installation were completed. By October 1940 enthusiasm had been revived and production of the Tornado and Typhoon reinstated, production deliveries of both being scheduled for the following year. A Tornado assembly line was laid down by Avro, the production model being intended to receive the Vulture V of 1980hp, with which both prototypes were reengined. The Vulture, meanwhile, was suffering various problems, such as connecting rod bolt failures, and as the Merlin possessed absolute priority, Rolls-Royce was forced to abandon the production of this X-type engine. This led to cancellation of the initial production batch of 201 Tornados, only one production example being completed and flown on 29 August 1941.
But this was fated to be the only production Tornado, for difficulties with the Vulture resulted in the decision to remove this power plant from the aero-engine development program, this decision also canceling production of the Tornado.
The Tornado weighed 8,200 lb. empty and 10,580 lb. loaded. Its maximum speed was 425 m.p.h. at 23,000 feet.
However, in February 1941, Hawker’s received a contract to convert a Tornado to take a 2210hp Bristol Centaurus CE.4S 18-cylinder air-cooled radial engine. Among the modifications required were a new center fuselage and engine mounting. The new prototype (HG641) was assembled from Tornado production components and flown for the first time on October 23, 1941. The first Centaurus installation had an exhaust collector ring forward of the engine from which a single external exhaust stack pipe led back under the root of the port wing. This arrangement soon proved unsatisfactory, so the oil-cooler duct was enlarged and led forward to the nose, while twin exhaust pipes led back from the front collector ring through this fairing to eject under the belly of the fuselage. A level speed of 421 m.p.h. was attained with the Centaurus-Tornado, and this was slightly higher than that attainable by the Sabre-powered Typhoon, but the Typhoon airframe could not be adapted to take the radial engine.
When a captured Focke-Wulf Fw 190A was examined late in 1941, numerous alterations to the British radial engine installation were made by Bristol, with considerable benefit to the test bed’s performance.
The second prototype Tornado (P5224) had, in the meantime, been completed, and the sole production Tornado (R7936) later played a useful role as a test-bed for deHavilland and Rotol contraprops.
The Centaurus Tornado continued flying in 1942 and it was the encouraging results that led to the Tempest II.

Hawker Tornado
Engine: Rolls Royce Vulture V, 1953 hp
Length: 32 ft 10 in / 10.01 m
Height: 14 ft 8 in / 4.47 m
Wingspan: 41 ft 11 in / 12.78 m
Wing area: 282.986 sq.ft / 26.29 sq.m
Max take off weight: 10670.0 lb / 4839.0 kg
Weight empty: 8379.0 lb / 3800.0 kg
Max. speed: 346 kt / 641 km/h / 398 mph
Service ceiling: 34908 ft / 10640 m
Wing loading: 37.72 lb/sq.ft / 184.0 kg/sq.m
Crew: 1

Hawker Hurricane

Hurricane IIA

The family tree of the Hurricane can be traced back to a ‘Fury monoplane’ proposal of 1933, then to be powered by the Rolls-Royce Goshawk evaporative-cooled power plant. Instead it was decided in early 1934 to adapt this design to incorporate the new PV.12 engine which Rolls-Royce had developed – and which was the direct forbear of the famous Merlin. From that time the airframe/engine combination bore so little relation to the Fury that it then became identified as the ‘Interceptor Monoplane’.

Hawker Hurricane Article

In 1933, Hawker‘s chief designer Sir Sidney Camm realised that something even better than the Fury was needed and the Hawker Fury monoplane was the result – a cantilever monoplane with fixed under-carriage and 660 h.p. Rolls Royce Goshawk engine. At this time 4 machine guns were considered adequate; but higher speeds reduced the time an enemy could be held in the pilot‘s gun sights and eventually plans were amended to accommodate 8 machine guns all mounted in the wings. The new Rolls Royce Merlin I was fitted and the aeroplane outstripped the original conception – it was no longer the Fury monoplane – the name Hurricane was chosen.

This finalised design was submitted to the Air Ministry in 1934, and in the following year a prototype was ordered to Specification F.36/34, and the Air Ministry asked for an armament of no less than eight machine-guns.

In 1934, the monoplane layout was still very new for combat aircraft and thick airfoils for monoplanes were much in vogue for structural rea-sons, if nothing else. Hurricane designer Sir Sydney Camm seemed to have had misgivings from the start. “When its design had gone beyond the point of no return,” he once admitted, “I had a sudden foreboding that it would be no good. Strength had to be an important factor in this ship, but I always wished that the wing had been thinner. If we had had more time, the Hurricane would have been the greatest aircraft of all time.” But if Hawker hadn’t frozen the design and gone ahead with mass production when it did, even without an official order. It was Hawker’s gamble in laying down a production line of 1,000 Hurricanes before the Air Ministry ordered such a vast quantity was available the Battle of Britain.

The Hawker engineer Frank Murdoch was responsible for getting the Hurricane into production in sufficient numbers before the outbreak of the war, after an eye-opening visit to the MAN diesel plant in Augsburg in 1936.

The prototype Hurricane K5083 flew on November 6, 1935 at Brooklands, piloted by Hawker’s chief test pilot, Flt.-Lt. “George” Bulman and powered by a 767kW Merlin ‘C’ engine. On landing he reported that it handled perfectly and was free from vices. Even at this date the retractable undercarriage was considered by many an extravagant novelty.

Hurricane prototype K5083 in early 1936

Advanced features such as an enclosed cockpit and retractable undercarriage were combined with traditional methods of construction using a tubular metal structure and fabric covering, meant that the Hurricane could be easily and rapidly produced in existing facilities.

In February 1936, the prototype Hurricane (as yet un-named), powered by an early Merlin C producing 990 hp and driving a Watts fixed-pitch two-bladed wooden propeller, was tested at the Aircraft and Armament Experimental Establishment at Martlesham Heath, giving service pilots their first opportunity to experience the performance.

Convinced that the RAF would buy the new fighter the Hawker company decided, in March 1936, to proceed with the production drawings and to make plans for large scale production. Three months later the Air Ministry confirmed that 600 Hurricanes were to be included in its expansion Plan F (which also provided for 300 Spitfires) to be delivered by March 1939. The target was missed by six months. There had been a succession of relatively minor but time-consuming problems with prototype development, especially related to the Merlin, and the early intention to fit the Merlin F (Mk.1) in the production Hurricane was changed to make use of the improved Merlin G (Mk.II), which required a redesign of the installation and the front fuselage profile before production could begin. The cockpit canopy also produced problems with five failures recorded on the prototype before a satisfactory design was evolved.

Convinced that the RAF would buy the new fighter the Hawker company decided, in March 1936, to proceed with the production drawings and to make plans for large scale production. Three months later the Air Ministry confirmed that 600 Hurricanes were to be included in its expansion Plan F (which also provided for 300 Spitfires) to be delivered by March 1939. The target was missed by six months. There had been a succession of relatively minor but time-consuming problems with prototype development, especially related to the Merlin, and the early intention to fit the Merlin F (Mk.1) in the production Hurricane was changed to make use of the improved Merlin G (Mk.II), which required a redesign of the installation and the front fuselage profile before production could begin. The cockpit canopy also produced problems with five failures recorded on the prototype before a satisfactory design was evolved.

The first production Hurricane I, LIS47, flew at Brooklands on October 12, 1937, fitted with an early example of the Merlin II and at a weight of 5459 lb (2476 kg), a contract for 600 having been placed in June 1936. This was increased to 1000 in November 1938.

The second aircraft was in the air on 18 October, and production deliveries then built up rapidly. Meanwhile, during 1936, the prototype had been fitted with the planned armament of eight Browning machine guns and first firing trials had been made. Design of a metal-covered wings was in hand, but to avoid production delays the Hurricane I retained the fabric-covered wing, in which the guns were grouped in two quartets, positioned to fire just outside the propeller disc and requiring no synchronisation gear. Each gun was provided with 300 rounds, and the two batteries were harmonised to converge at 650 yards (594m), although with experience this distance was to be reduced eventually to 200 yards (183m).

Hawker Hurricane Mk 1

Although of cantilever monoplane configuration, its construction was typical of the Fury from which it stemmed, and even its wings were fabric-covered in early Mk Is, with a metal leading edge and trailing-edge flaps. The tailwheel-type landing gear had hydraulically retractable main units of wide track. Armament of production Mk Is comprised four 7.7mm Browning machine-guns in each wing, making this the RAF’s first eight-gun fighter. Designated the Hurricane I, it was outfitted with a Rolls-Royce Merlin II or III engine, fabric-covered wings, and a wooden prop. It lacked armor and selfsealing fuel tanks.

In Yugoslav, Ikarus and Zmaj shared the order for the production of Hurricane MK1.

A second major version of the Hurricane made its first flight on 11 June 1940 and, as the Hurricane IIA powered by a Merlin XX, would begin to reach the Squadrons on 4 September 1940. Improvements included wing alterations for increased armament, redesigned engine mount, strengthened fuselage, and tanks protected with self-sealing rubber.

The Hurricane I was improved with an armoured bulkhead introduced forward of the cockpit and, when Hawker Aircraft’s second production batch began leaving the assembly line in September 1939, a bullet-proof windscreen had been standardised. This batch also adopted the Merlin III which features a shaft capable of taking either Rotol or de Havilland three-bladed constant speed propeller. While some Hurricanes were produced during 1939 with the DH two-position propeller, a major conversion programme was started on 24 June 1940 to fit the Rotol constant speed unit which allowed the pilot to select optimum power for the various stage of flight. Significantly improving the Hurricane I’s climb performance, Rotol propellers had been fitted to all Hurricanes by mid-August 1940. With the 81th Hurricane of the second batch, the fabric covered wing gave place to an all metal stressed skin wing and, on 2 February 1940 the first Hurricane with rear armour protection for the pilot was flown.

By the end of 1939, the RAF had received more than 600 Hurricane Is and production was at a rate of 100 a month. Gloster began Hurricane production flying its first Hurricane I at Hucclecote on 20 October 1939.

No.111 Sqn RAF August 1938

By December 1937 No. 111 Squadron at Northolt was beginning to re-equip with the type, and were fully equipped by February 1938. Early in the new year made front page news when S/Ldr. J. W. Gillan, Officer Commanding lll Sqn., flew from Edinburgh to Northolt (assisted by a tail wind) at an average speed of 408 m.p.h.

By July 1939, twelve regular squadrons were flying the Hurricane I, to be followed by six Auxiliary Air Force squadrons. By the outbreak of war in 1939, 500 Hurricanes had been delivered and by August 7, 1940, when the Battle or Britain started, there were 32 Hurricane squadrons as against 19 Spitfire squadrons. By that time, the Hurricane had already been in action in France, Norway and Malta. At the outbreak of war in September, 1939, the Royal Air Force returned to France equipped with Hurricanes. Before this, Hurricanes of No. 46 Sqn. took part in the fighting in Norway, brought into action by the aircraft carrier “Glorious”. When the order came to evacuate, the Squadron flew all its Hurricanes on to the “Glorious” without arrestor gear rather than resort to destroying them, but this effort was in vain when the carrier was subsequently sunk. Similarly, Hurricanes flown from H.M.S. Argus reinforced the Gladiators in the Battle of Malta. In the Battle of Britain, the Hurricane bore the brunt of the fighting.

Hurricanes downed more enemy aircraft than did the Spits in the Battle, and the highest-scoring RAF pilot in the Battle, a Polish sergeant named Josef Frantitek (with a score of 17, all in a single month) flew Hurricanes.

One of the significant statistics of the Hurricane’s contribution to this hard-fought battle was the fact that these aircraft destroyed more enemy aircraft than the combined total of all other defence systems, air or ground. Even that factor must be equated with the information that at the beginning of the battle (on 8 August 1940) approximately 65% more Hurricanes than Spitfires (2,309 to 1,400) had been delivered to the RAF’s Fighter Command.

After the Russian invasion of Finland in 1940, slowly reinforcements began to arrive for the Finnish air force. The first to come were 5 Gloster Gladiators, 12 Hurricanes, 17 Lysanders and 24 Blenheims, all from Britain. After that, 76 Morane-Saulnier and Koolhoven F.K. fighters arrived from France. Italy sent 17 Fiat fighters, Sweden 12 Gloster Gladiators, and the USA 44 Brewster Buffalo, of which however only 5 reached Finland in time. Even the Union of South Africa sent 25 Gloster Gladiators. Pilots and ground personnel from a number of countries also volunteered to assist them.

After 1940, Hurricanes served largely in the Middle East and North Africa, with a distinctive sand filter under the nose to protect the Merlin’s innards. They were tried as night fighters over Britain after the Luftwaffe switched to night raids, but the night-fighting Hurricanes had generally poor success.

The aeroplane had now changed slightly from the early production mark, among other modifications, a 3-blade controllable pitch airscrew was fitted. A ventral fin faired the fixed tail wheel to improve handling qualities and metal had replaced fabric covering on the wings. Subsequent Hurricane versions included the Mk IIA with Merlin XX and eight guns; Mk IIB with 12 guns; and Mk IIC with four 20mm cannon. Mk IID with two 40mm Vickers ‘S’ guns and two 7.7mm guns (plus additional armour for low attack) were used extensively in the Western Desert. The final production version was the Mk IV with a wing able to accept armament comprising two Browning machine-guns plus two 40mm guns, or eight rocket projectiles, or two 110kg or 225kg bombs, or long-range fuel tanks. The Hurricane V (only two built) was powered by a Merlin 27 or 32 engine.

The Hurricane Mark II first flew on June 11th, 1940 with Merlin XX two-stage supercharged engine. A special set of mainplanes were made to accommodate the various armament. The Mk. IIA retained the eight Brownings. On the Mk. IIB these were increased to no less than 12 guns. Four 20 mm. Hispano cannons replaced the rifle-calibre guns on the IIC, and on the Mk. IID two 40 mm. Vickers cannon with two Brownings firing tracer ammunition for sighting. To increase the range, 90 gallon drop tanks were suspended below the wings on the IIC and armed with 4×20 mm. cannon the Hurricane a familiar sight with its Vokes sand filter during the North African campaign.

In August 1941 Great Britain decided to lend fighter plane support to Russia. British 151st Wing was set up in Leconfield near York, to train Soviet aircrews in the assembly, maintenance and operation of the fighters. Then Nos 81 and 134 Squadrons, comprising 39 Hurricane Mk.IIB, were shipped to the Soviet Union along with their pilots and ground personnel. The old British aircraft carrier Argus transported 24 of the Hurricanes, and the other 15 were packed and sent along on other vessels as deck cargo. The convey put to sea from Iceland on 21 August 1941 and docked at Murmansk on August 28. Here the 24 Hurricanes took off from Argus and landed at Viange airport about 15 miles away, which served 151st Wing as their main airbase during their stay in the Soviet Union.

On Sunday 3 August 1941, the first aerial victory won by a British Hurricane catapulted from a CAM ship took place when Lt. Robert Everet of 804 Sqn, based on the steamer Maplin, shot down a Focke-Wulf Fw 200C Condor of German 40 Sqn, 1st Bomber Wing in the North Atlantic. Instead of making a sea landing near his mother ship, the pilot decided to fly the 300 miles to Scotland, and landed there at Loch Earn.

CAM freighter carrying a Sea Hurricane

By 1942, most Hurricanes had been switched to ground attack, with a powerful variety of weapons: 12 Brownings; or four 20mm cannon that slowed you down by 30 mph when you fired them; or a pair of Brownings plus two 40mm cannon with just 20 armor-piercing rounds. Another variant was the “Hurribomber”, with racks for two 250-pounders, or even two 500-pounders, sometimes delivered by skip-bombing. Rocket rails were also commonly fitted. In the Far East, Burma and India, the Hurricane remained the principal British fighter opposing the Japanese right up to the war’s end. Some 3,000 Hurricanes (one in five of all built) were given to the Soviet Union, most shipped by convoy around the North Cape to Murmansk.

Hawker Hurricane MkII converted by the Soviets with a back seat and machine gun position.

After early experience of deck landing Hurricanes, an arrestor hook was fitted and in this form was known as the Sea Hurricane Mk. IB. Sea Hurricanes joined the Royal Navy in January 1941 and became the first carrier-based British single-seat monoplane fighter when taken to sea by HMS Furious in July 1941. Under the ‘Catfighter’ scheme, Sea Hurricane IA were equipped for catapult launch from the decks of CAM merchant ships (catapult-equipped merchantmen) to counter the threat posed by Germany’s Focke-Wulf Fw 200 Condors, introduced in the spring in 1941. Only the Mk IA was specially built. The approximate figure of 800 Sea Hurricanes which entered service included 50 Mk IA and about 750 conversions of Mk II and Canadian-built aircraft.

These were 35 ordinary merchant ships that had been modified to carry a Hurricane on a rocket launch rig on the bow. These CAM ships, carrying ordinary cargo as well, accompanied the great convoys sailing from Britain to Russia and the Mediterranean, and from Canada to Britain. The Hurricats were assigned to convoy defense against the Luftwaffe’s Focke-Wulf Condor long-range, four-engine reconnaissance bombers, which were not only attacking convoys, but tracking them for U boats and other bomber units. If a Hurricat pilot was lucky, he could make it back to shore after launch and combat if not, he had to ditch (not recommended, since the Hurri-cane invariably turned over and sank) or else bail out over the convoy.

Hawker Hurricane CAM Article

Apart from its role as a purely fighter aeroplane, the Hurricane served as a fighter bomber with two 250 lb. and later two 500 lb bombs below the wings. The aeroplane was also used for night fighting and pioneered the use of rocket projectiles until the advent of the Typhoon. In this guise it was known as the Mk. IV.

Mention must be made of at least one interesting experiment. A supplementary wing of identical shape and area was fitted to a standard Mk. I Hurricane to enable it to take off with a much greater load. This wing was released in flight. A long series of tests were conducted but the project did not proceed beyond the experimental stage. Another version of the Hurricane was equipped with floats.

During the Second World War Gloster built 2,750 Hurricanes and 3,330 Typhoons,

The Hurricane was eventually replaced on Hawker’s production lines by the Typhoon, the Tempest, the Fury and the Sea Fury.

Hurricane evolution effectively stopped at the Mark IV.

In November 1938, the Canadian Car and Foundry Company was awarded a contract to produce Hawker Hurricanes for the RAF at its Fort William plant. The initial order was for forty aircraft (P5170 to P5209) to Mk 1 specification with British made Rolls Royce Merlin III engines and eight .303 Browning machine guns. These models depended almost entirely on British materials such as steel tubing, aluminium sheeting and metal castings which were formed, pressed and machined at Fort William, since the Canadian aircraft industry did not at that time have the capability to produce these items from scratch.

With the outbreak of war, shipping delays and losses created problems with such a system and as late as 1941 shortages of imported British materials reduced production considerably. Mr G C Kemp, a foreman at that time, recollects that at one point a delay in the arrival of Merlin engines was overcome by flying as many as thirty Fairey Battles into Fort William, where the engines were removed and fitted into the Hurricanes. In time, with new Canadian sources of supply and the introduction of the Packard Merlin engine from the US, production rose to reach a peak of 700 aircraft in 1942. In all, between January 1940, when the prototype (P5170) flew, and June 1943, when the last Hurricane left the plant at Fort William, 1,451 aircraft of various marks were built, representing some 10% of all Hurricanes produced and almost half of Can Car’s total production during the war years.

The Hurricane 1 was in many ways a transitional design between the wood, metal and fabric biplanes of the 1920s and 1930s and the metal skinned monoplane fighters of the 1940s. It incorporated a metal frame with a combination of wooden fairing and fabric over the fuselage and fabric covering the wings. All of the CCF built Hurricanes however had aluminium covered wings and indeed, when Mr A D Norton, head of the Tool Design Section at Can Car, visited the Hawker works in England in 1939, he found the development of the metal skinned wings less advanced than at Fort William. Apart from that, the basic structure of the Hurricane changed little in its lifetime. Some were fitted to carry bombs, some had catapult fittings, others had arrester gear, some were tropicalised and at least two were fitted with skis by the RCAF. The normal elements used to differentiate the variants, however, were powerplant and armaments.

The initial order for forty machines was renewed and in total 160 Mk 1 aircraft were built in five different batches. Most of these seem to have been sent directly to Britain, where they were distributed as the need arose rather than being assigned by batch to any one squadron, this being made possible by the inter-changeability of components among British and Canadian-built aircraft. Twenty were delivered before the Battle of Britain and some of these participated in the fierce aerial fighting of August and September 1940.

The majority of the Hurricanes built by CCF at Fort William were Mk X or Mk XII variants, equivalent to the British built 1 and IIB, and amounting to 900 aircraft or 62% of the total. Both were equipped with Packard engines, the Merlin 28 in the case of the Mk X and the Merlin 29 in the Mk XII, while the latter carried twelve Brownings compared to the eight of the Mk X. Most of the Hurricane Xs were initially sent to Britain, but
some were later tropicalised and used in India. After many requests, about thirty of these aircraft were also released for use by the RCAF in Canada.

Those sent to Britain seem to have been modified quite regularly as the Hurricane evolved into its intruder and ground attack role. Many with serial numbers between AM270 and AM369, for example, built as Mk Xs were later designated IIB or IIC, presumably because of changes in armaments and the addition of external bomb racks or fuel tanks rather than the wholesale replacement of the Packard Merlin with its Rolls Royce equivalent, although, of course, the latter may have applied in some cases also. With some, multiple conversions took place. Hurricane AM280, for example, started life as a Mk X but appears in late 1941 or early 1942 on the books of 1 Squadron as a Mk X converted to IIB configuration. Later in 1942 and 1943 it is referred to variously as a Mk X/11C with 534 Squadron and a “Mk X, modified with four cannon wings with 3 Squadron.

Unlike the Mk Xs, the Hurricane XII’s (RCAF 5376 to 5775) with their Merlin 29 engines and twelve Browning guns armament remained in Canada with the RCAF, flying defensive patrols along the east and west coasts, but without becoming involved in combat. This applies also to a batch of fifty Hurricane XIIAs, built as Sea Hurricanes for the Fleet Air Arm, but subsequently released for service with the RCAF. These aircraft were similar to the Mk XII in that they had Merlin 29 engines, but were fitted with eight gun Mk 1 or Mk X wings.
The situation with the Mk XII variants is complicated by the fact that some of the later aircraft shipped to Britain without engines, instruments or armament were fitted with Merlin XX engines and either twelve Browning or four cannon wings and designated Mk 1IB/XII or IIC/XII although during construction in Canada they were nominally IIB or IIC. This applied to aircraft of the JS219 to JS468 batch which began to appear in Britian in 1942 to be used in intruder activities or as night fighters with the Turbinlite squadrons. Others of this group served with various squadrons in the Middle East and India.

The final four batches of Hurricanes (PJ660 to P.1695, PJ711 to PJ758, PJ779 to PJ813 and PJ842 to PJ872), built to Mk IIC specifications, were also intended for shipping to Britain for the fitting of engines, instruments and armament. Although some doubt has been expressed as to whether or not these were actually constructed, aircraft with serials from the second, third and fourth groups are recorded as serving in India in 1943 and 1944, flying escort to bombing raids or involved in low level fighter bomber activity over Burma.

Hurricane production continued until 1944. In all, Hawker produced 10,030, supplemented by 2750 from Gloster, and 1451 from Canada.

More than 4,000 Hurricanes were supplied to other air forces, including Belgium, Canada, Egypt, Eire, Finland, India, Persia, Poland, Portugal, Romania, South Africa, the Soviet Union, Turkey, and Yugoslavia.

Replica:
Flying Legends Hurricane
Sindlinger Hawker Hurricane

Gallery

Prototype
Engine: 767kW Merlin ‘C’
Weight: 5672 lb / 2572 kg
Speed: 315 mph / 506 kph at 16,200 ft / 4957 m with 6 lb/sq.in boost
TO run: 800 ft / 245 m
T/O speed: 81 mph / 130 kph
Time to 15,000 ft / 4570 m: 5.7 min
Time to 20,000 ft / 6100 m: 8.4 min
Service ceiling: 34,500 ft / 10,515 m
Est absolute ceiling: 35,400 ft / 10,800 m

Mk I
Engine: Rolls-Royce Merlin II or III, 990-1030 hp
Prop: Rotol 3 blade wood
Length: 31.4 ft. (9.55 m)
Height: 13 ft. 11 in
Wing span: 40 ft. (12.2 m)
Wing area: 257.5 sq. ft
MAUW: 6600 lb
Weight empty: 4,670 lb. (2,118 kg)
Max speed 325 mph @ 20,000 ft
Service ceiling 36000 feet.
Initial climb rate 2,950 fpm
Range: 460 miles (740 km)
Armament: 8 x 7.7mm / 0.303in Browning machine-guns
Bomb load: 1,000 lb. (450 kg)
Crew: 1

Hurricane I
Engine: Rolls-Royce Merlin II, 990hp
Prop: 2 blade wood fixed pitch
Wing span: 40 ft. (12.2 m)
Wing area: 257.5 sq. ft
Length: 31.4 ft. (9.55 m)
Height: 13 ft. 11 in
Weight empty: 4,732 lb. / 2,146 kg
Normal loaded weight: 6056 lb / 2747 kg
MTOW: 6202 lb / 2813 kg
Fuel capacity: 97 ImpGal / 441 lt
Range: 680 miles / 1094 km at 275 mph / 442 kph at 15,000 ft / 4575 m
Endurance: 4.2 hr at econ cruise
Econ cruise: 162 mph / 261 kph
Max speed 312 mph / 502 kph @ 20,000 ft
Time to 15,000 ft / 4575m: 7 min
Service ceiling 33,000 ft / 10,058m
TO to 50 ft / 15.2m norm wt: 1800 ft / 549 m
TO to 50 ft / 15.2m max wt: 1890 ft / 576 m
Armament: 8 x 7.7mm / 0.303in Browning machine-guns
Crew: 1

Hurricane II
Engine: One Rolls-Royce Merlin XX, 1,030 hp at sea level, 1,460 hp at 6,250ft in M gear and 1,435hp at 11,000ft in S gear.
Propeller: Rotol three-bladed constant speed 11 ft 3 in diameter.
Span, 12.2 m / 40 ft 0 in
Length, 9.8 m / 32 ft 3 in
Overall height, tail down, one blade vertical, 13 ft 3 in
Wing area, 24.0 sq.m / 258.33 sq ft
Weight empty: 4,670 lb. (2,118 kg).
Max take-off weight: 3540 kg / 7804 lb
Fuel capacity, 69 Imp gal in two wing tanks, 28 Imp gal in res fuselage tank, total 97 Imp gal.
Optional fuel: two 45 Imp gal drop or 90 Imp gal fixed ferry tanks under wings.
Max speed: 316 mph. (508 kph)
Ceiling: 10850 m / 35600 ft
Range w/max.fuel: 740 km / 460 miles
Undercarriage track, 7 ft 10 in
Aspect ratio, 62:1
Dihedral, 35 deg on outer wing panels
Crew: 1.
Armament: 4 x 20mm cannon.
Bomb load: 1,000 lb. (450 kg)

Hurricane IIA
Engine: Rolls-Royce Merlin XX, 1260 hp
Time to 20,000 ft / 6095 m: 8.2 min
Max speed: 342 mph / 550 kph at 22,000 ft / 6705 m
Armament: 12 mg or 4 cannon

Mk IIB
Engine: RR Merlin 25, 1280 hp.
Wing Span: 40 ft
Length: 32 ft 3 in
Height: 13 ft 1 ft
Tare weight, 5,467 lb
Empty equipped weight, 6,266 lb
Normal loaded weight, full armament and internal fuel, 7,233 lb.
Max speed, 328 mph at 18,000 ft clean, 310mph with tropical filter
Initial rate of climb, 2,950 ft/min clean, 2,800 ft/min with tropical filter
Time to 15.000 ft, 55 min. to 25,000 ft, 95 min
Service ceiling, 36,000 ft
Range, 465 mls at 177 mph clean, 935 mls with two 45 Imp gal drop tanks, 436 mls clean with tropical filter.
Armament: Twelve BSA-built Browning machine guns of 0.303-in calibre with a total of 3,988 rounds in 12 magazines (5,238 rounds in some aircraft).
Provision for two 250-lb or 500-lb bombs.

Mk IIC
Max speed, 327 mph at 18,000 ft clean, 301 mph with tropical filter
Initial rate of climb, 2,750 ft/min clean, 2,400 ft/min with tropical filter
Time to 15,000 ft, 6 min, to 25,000 ft, 10 min
Service ceiling, 35,600 ft
Range, 460 mls at 178mph clean, 920 mls with two 45 Imp gal drop tanks, 426 mls clean with tropical filter.
Tare weight, 5,658 lb
Empty equipped weight, 6,577 lb
Normal loaded weight, full armament and internal fuel, 7,544 lb
Max overload weight with drop tanks, 8,044 lb
Armament: Four Hispano Mk I or Mk II cannon of 20-mm capacity with 90 rpg.
Provision for two 250-lb or 500-lb bombs under wings.

Mk IID
Armament: two 40mm Vickers ‘S’ guns and two 7.7mm guns

Mk IV
Armament: two Browning machine-guns plus two 40mm guns, or eight rocket projectiles, or two 110kg or 225kg bombs, or long-range fuel tanks.

Hurricane V
Engine: Merlin 27 or 32 engine.
No built: 2

Sea Hurricane IA

Sea Hurricane Mk II C
Engine: Rolls Royce Merlin XX, 1262 hp
Length : 32.251 ft / 9.83 m
Height: 13.091 ft / 3.99 m
Wingspan: 39.993 ft / 12.19 m
Wing area: 257.475 sq.ft / 23.92 sq.m
Max take off weight: 8101.2 lb / 3674.0 kg
Weight empty: 5880.7 lb / 2667.0 kg
Max. speed: 297 kt / 550 km/h
Cruising speed: 184 kt / 341 km/h
Service ceiling: 35597 ft / 10850 m
Cruising altitude: 20013 ft / 6100 m
Wing load: 31.57 lb/sq.ft / 154.0 kg/sq.m
Maximum range: 843 nm / 1561 km
Range: 400 nm / 740 km
Crew: 1
Armament: 4x 20mm MG

Canadian Car and Foundry Co Hurricane Mk 1
Engine: British made Rolls Royce Merlin III
Armament: eight .303 Browning machine guns.

Canadian Car and Foundry Co Hurricane Mk X (British built Mk 1)
Packard Merlin 28
Armament: 8 x Brownings

Canadian Car and Foundry Co Hurricane Mk XII ( British built Mk. IIB)
Packard Merlin 29
Armament: 12 x Brownings

Canadian Car and Foundry Co Sea Hurricane XIIA
Engine: Merlin 29
Armament: eight gun

Mk IIB/XII
Merlin XX

Mk IIC/XII
Merlin XX

Hawker Hornet / Hawker Fury I

Fury

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.

Hawker Hornet

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

Hawker Hornet
Hawker Fury

Hawker F.20/27

This experimental single-seat interceptor fighter designed by Sydney Camm to meet the requirements of Specification F.20/27, was flown in August 1928 with a 450hp Bristol Jupiter VII radial. Of metal construction with sharply staggered single-bay wings and a twin-Vickers gun armament, the prototype was re-engined with a 520hp Mercury VI in May 1930. It demonstrated a maximum level speed of 325km/h. By this time the F.20/27 specification had prompted Hawker to initiate development of a more advanced fighter as a private venture, and this, owing much to the F20/27, was to emerge as the Hornet in 1929.

F.20/27
Engine: 520hp Mercury VI
Max take-off weight: 1429 kg / 3150 lb
Empty weight: 977 kg / 2154 lb
Wingspan: 9.14 m / 29 ft 12 in
Length: 7.17 m / 23 ft 6 in
Height: 2.87 m / 9 ft 5 in
Wing area: 21.18 sq.m / 227.98 sq ft
Max. speed: 325 km/h / 202 mph

Hawker Hind

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

Hawker Osprey / Nohab

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)

Hawker Hartebeeste / Hartbee / Hartbees

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.

Hawker Hotspur

When, in 1935, Specification F.9/35 was issued for a two-seat interceptor fighter to replace the Demon, both Hawker and Boulton Paul tendered proposals for aircraft fitted with the Boulton Paul turret mounting four 0.303-in (7,7-mm) machine guns. Hawker’s submission was based on redesign of the Henley light bomber, prototype construction of which had just commenced. Like the Henley, it utilised standard Hurricane outer wing panels. Dubbed Hotspur, the prototype (K8309) of the two-seat fighter was not flown until 14 June 1938, and then with only a wooden mock-up of the turret and with ballast equivalent to the weight of armament. Powered by a 1,030 hp Rolls-Royce Merlin II, the Hotspur proved faster than the competitive Boulton Paul Defiant, but as Hawker and its parent Group were fully committed to production of the Hurricane, no effort was made to bring the prototype Hotspur up to representative Service standard and development was discontinued, the aircraft subsequently being utilised for flap and dive brake development.

Max take-off weight: 3470 kg / 7650 lb
Empty weight: 2631 kg / 5800 lb
Wingspan: 14.59 m / 47 ft 10 in
Length: 11.01 m / 36 ft 1 in
Height: 4.37 m / 14 ft 4 in
Wing area: 31.77 sq.m / 341.97 sq ft
Max. speed: 509 km/h / 316 mph

Hawker Henley

The Henley was designed to an Air Ministry requirement for a two-seat-high-performance light bomber with good enough performance to be used as a dive bomber for close air support.

The prototype first flew in March 1937.

Despite its promise, its role was changed to that of target towing. Four hundred were ordered, but only 100 Merlin II and 100 Merlin III-engined Henleys were built at the Gloster works. The type proved ill-suited to the task, with many engine failures due to a cooling system which performed best at high airspeeds not suitable for target towing. They ended their short careers towing the larger drogues for training anti-aircraft gun crews. They were withdrawn from service in 1942.

According to Hawker records two Henleys were used as engine test beds for Vulture and Griffon engines and one was tropicalised.

Engine: 1 x Rolls-Royce Merlin II, 1016 hp / 768kW
Wingspan: 14.59 m / 47 ft 10 in
Length: 11.1 m / 36 ft 5 in
Height: 4.46 m / 14 ft 8 in
Wing area: 31.77 sq.m / 341.97 sq ft
Max take off weight: 3845 kg / 8477 lb
Empty weight: 2725 kg / 6008 lb
Wing loading: 24.81 lb/sq.ft / 121.00 kg/sq.m
Service Ceiling: 8230 m /27000 ft
Max. speed: 204 kts / 438 km/h /272 mph
Cruising speed: 378 kph
Range: 826 nm / 1529 km / 950 miles
Crew: 2

Hawker Hector

Prototype

British Army co-operation biplane. The Hawker Hector was an 600kW / 805 hp Napier Dagger air-cooled and supercharged powered derivative of the Hawker Hart produced to meet a 1935 specification for a replacement for the Hawker Audax, itself a development of the Hart.

The H type Dagger IIIMS 24-cylinder gave the Hector a distinctive nose profile, while other modifications included an upper wing with straight leading edge, a tail wheel in place of the original skid and a canted ring for the Lewis machine gun in the rear cockpit. A 0.303 in (7.7 mm) Vickers was fitted in the port side of the nose, and two 51 kg (112 lb) bombs could be carried below the lower wings.

The prototype Hector, a converted Hart which first flew on February 14, 1936, was followed by 178 Westland built production machines, the first of which entered service in February 1937.

At the time of a Finnish evaluation, the Hector equipped seven RAF army co-operation squadrons, although the Finns were also advised that it was intended to start replacing the Hectors in RAF service in 1938. The Ilmavoimat / Maavoimat / VL Team expressed considerable disbelief among themselves that in early 1938 the RAF was still flying an aircraft reminiscent of the first World War, particularly in light of the German aircraft designs they were also looking at. Their initial conclusion was that the aircraft was unreliable, obsolete and would be ineffective in its intended role. The Hector was eliminated from the evaluation with no further consideration.

Only a handful of Hectors were ever flown in anger, raiding German positions in occupied France in May 1940. After the Lysanders started entering service, the Hectors were transferred to RAF Auxiliary Air Force squadrons; 613 Squadron used theirs to attack German troops advancing through northern France in May 1940. Two aircraft were lost in combat over Calais, before the squadron was evacuated. Hectors were used by the RAF from 1940 as target-towers, and for towing the General Aircraft Hotspur training gliders. The type was deeply unpopular with ground crews due to the complicated nature of the engine, which had 24 cylinders, with 24 spark plugs and 48 valves, all of which required frequent maintenance.

Britain sold the Irish Free State 13 of the Hectors after the Dunkirk Evacuation. In general they were in poor condition. They were sold by the British War Office to the Irish Free State upon requests for aircraft. The Irish military were wholly unprepared for major warfare, but still relied almost totally on military supplies from Britain. The defence of Ireland was also in the British interest, but with the Battle of Britain raging in the skies, could afford to sell the Irish Government nothing better than the Hector.

Engine: 1 x Napier Dagger III MS “H”, 600kW / 805 hp
Max take-off weight: 2227 kg / 4910 lb
Empty weight: 1537 kg / 3389 lb
Wingspan: 11.26 m / 36 ft 11 in
Length: 9.09 m / 29 ft 10 in
Height: 3.17 m / 10 ft 5 in
Wing area: 32.14 sq.m / 345.95 sq ft
Wing loading: 14.15 lb/sq.ft / 69.0 kg/sq.m
Max. speed: 163 kts / 301 km/h / 187 mph
Ramge: 300 miles
Service Ceiling: 7315 m / 24000 ft
Armament: 1 x 7.7mm / 0.303in Vickers Mk.V machine-guns (forward firing), one rear-firing 303 in (7.7 mm) Lewis gun mounted in the rear cockpit
Bombload: 2 x 51kg bombs
Crew: 2