The Hawker Tempest is a British fighter aircraft primarily used by the Royal Air Force (RAF) in the Second World War. The Tempest, originally known as the Typhoon II, was an improved derivative of the Hawker Typhoon, intended to address the Typhoon's unexpected deterioration in performance at high altitude by replacing its wing with a thinner laminar flow design. Having diverged considerably from the Typhoon, it was chosen to rename the aircraft Tempest. The Tempest emerged as one of the most powerful fighters of World War II and was the fastest single-engine propeller-driven aircraft of the war at low altitude.
|Tempest V prototype HM595 with early "car door" cockpit structure and small tail unit.|
|Manufacturer||Hawker Aircraft Limited|
|First flight||2 September 1942|
|Primary users||Royal Air Force|
Indian Air Force
Royal New Zealand Air Force
Pakistan Air Force
|Developed from||Hawker Typhoon|
|Developed into||Hawker Sea Fury|
Upon entering service in 1944, the Tempest was used as a low-level interceptor, particularly against the V-1 flying bomb threat, and as a ground attack platform, in which it supported major events such as Operation Market Garden. Later, it successfully targeted the rail infrastructure in Germany and Luftwaffe aircraft on the ground, as well as countering such attacks by German fighters. The Tempest was effective in the low-level interception role, including against newly developed jet-propelled aircraft such as the Messerschmitt Me 262.
The further-developed Tempest Mk.II did not enter service until after the end of hostilities. It had several improvements, including being tropicalised for combat against Japan in South-East Asia as part of the Commonwealth Tiger Force.
Design and developmentEdit
During development of the earlier Hawker Typhoon, the design team, under the leadership of Sydney Camm, had already planned out a series of design improvements; these improvements cumulated in the Hawker P. 1012, otherwise known as the Typhoon II or Thin-Wing Typhoon. Although the Typhoon was generally considered to be a good design, Camm and his design team were disappointed with the performance of its wing, which had proved to be too thick in its cross section, and thus created airflow problems which inhibited flight performance, especially at higher altitudes and speeds where it was affected by compressibility. The Typhoon's wing, which used a NACA 4 digit series wing section, had a maximum thickness-to-chord ratio of 19.5 per cent (root) to 12 per cent (tip), in comparison to the Supermarine Spitfire's 13.2 per cent tapering to 6 per cent at the tip, the thinner design being deliberately chosen to reduce drag. In addition, there had been other issues experienced with the Typhoon, such as engine unreliability, insufficient structural integrity, and the inability to perform high altitude interception duties.
In March 1940, engineers were assigned to investigate the new low–drag laminar flow wing developed by NACA in the United States, which had been used in the new North American P-51 Mustang. A laminar flow wing adopted for the Tempest series had a maximum thickness-to-chord ratio of 14.5 per cent at the root, tapering to 10 per cent at the tip. The maximum thickness of the Tempest wing was set further back at 37.5 per cent of the chord versus 30 per cent for the Typhoon's wing, reducing the thickness of the wing root by five inches on the new design. The wingspan was originally greater than that of the Typhoon at 43 ft (13.1 m), but the wingtips were later "clipped" and the wing became shorter; 41 ft (12.5 m) versus 41 ft 7 in (12.7 m).
The wing planform was changed to a near-elliptical shape to accommodate the 800 rounds of ammunition for the four 20 mm Hispano cannons, which were moved back further into the wing. The new wing had greater area than the Typhoon's,[nb 1] however, the new wing design sacrificed the leading edge fuel tanks of the Typhoon: to make up for this loss in capacity, Hawker engineers added a new 21 in (53 cm) fuel bay in front of the cockpit, with a 76 Igal (345 l) fuel tank. In addition, two inter-spar wing tanks, each of 28 Igal (127 l), were fitted on either side of the centre section and, starting with late model Tempest Vs, a 30 Igal (136 l) tank was carried in the leading edge of the port wingroot, giving the Tempest a total internal fuel capacity of 162 Igal (736 l).
Another important feature of the new wing was Camm's proposal that the radiators for cooling the engine be fitted into the leading edge of the wing inboard of the undercarriage. This eliminated the distinctive "chin" radiator of the Typhoon and improved aerodynamics. A further improvement of the Tempest wing over that of the Typhoon was the exceptional, flush-riveted surface finish, essential on a high performance laminar flow airfoil. The new wing and airfoil, and the use of a four-bladed propeller, acted to eliminate the high frequency vibrations that had plagued the Typhoon. The design team also chose to adopt the new Napier Sabre IV engine for the Tempest, drawings of which had become available to Hawker in early 1941.
In February 1941, Camm commenced a series of discussions with officials within the Ministry of Aircraft Production on the topic of the P.1012. In March 1941 of that year, clearance to proceed with development of the design, referred to at this point as the Typhoon II, was granted. At this point, work was undertaken by a team of 45 draughtsmen at Hawker's wartime experimental design office at Claremont, Esher to convert the proposal into technical schematics from which to commence manufacture. In March 1941, the Air Ministry issued specification F.10/41 that had been written to fit the aircraft. By October 1941, development of the proposal had advanced to the point where the new design was finalised.
On 18 November 1941, a contract was issued by the Air Ministry for a pair of prototypes of the "Typhoon Mark II"; the new fighter was renamed "Tempest" on 28 February 1942.[nb 2] Complications were added to the Tempest program by external factors in the form of engine issues: the Rolls-Royce Vulture engine and corresponding Hawker Tornado aircraft which was being developed in parallel were both terminated. Due to this previous experience on other programs, the Air Ministry was sufficiently motivated to request that a total of six Tempest prototypes be built using different engines so that, if a delay hit one engine, an alternative powerplant would already be available. This measure turned out to be prudent, as engine development was not trouble-free on some of the variants of the Tempest.
The six prototypes were built as a single Mk.I, HM599, powered by a Sabre IV, two Mk.IIs (LA602 and LA607) equipped with the Centaurus IV, a Mk.III (LA610) with a Griffon IIB, a Mk.IV (LA614) with a Griffon 61, and a Mk.V (HM595) with the Sabre II. The Tempest Mk.I featured other new features, such as a clean single-piece sliding canopy in place of the car-door framed canopy, and it used wing radiators instead of the "chin" radiator.[nb 3] Due to development difficulties with the Sabre IV engine and its wing radiators, the completion of the Mk.I prototype, HM599, was delayed, and thus it was the Mk.V prototype, HM595, that would fly first.
On 2 September 1942, the Tempest Mk.V prototype, HM595, conducted its maiden flight, flown by Philip Lucas from Langley, Berkshire, England. HM595, which was powered by a Sabre II engine, retained the Typhoon's framed canopy and car-style door, and was fitted with the "chin" radiator, similar to that of the Typhoon. It was quickly fitted with the same bubble canopy fitted to Typhoons, and a modified fin that almost doubled the vertical tail surface area, made necessary because the directional stability with the original Typhoon fin had been reduced over that of the Typhoon by the longer nose incurred by the new fuel tank. The horizontal tailplanes and elevators were also increased in span and chord; these were also fitted to late production Typhoons. Test pilots found the Tempest a great improvement over the Typhoon in performance; in February 1943 the pilots from the A&AEE at Boscombe Down reported that they were impressed by "a manoeuvrable and pleasant aircraft to fly with no major handling faults".
On 24 February 1943, the second prototype HM599 first flew, representing the "Tempest Mk.I" equipped with the Napier Sabre IV engine; this flight had been principally delayed by protracted problems and slippages encountered in the development of the new Sabre IV engine. HM599 was at first equipped with the older Typhoon cockpit structure and vertical tailplane. The elimination of the "chin" radiator did much to improve overall performance, leading to the Tempest Mk.I quickly becoming the fastest aircraft that Hawker had built at that time, having attained a speed of 466 mph (750 km/h) during test flights.
On 27 November 1944, the Tempest Mk.III prototype, LA610, conducted its first flight; it was decided to discontinue development work on the Mk.III, this was due to priority for the Griffon engine having been assigned to the Spitfire instead.[nb 4] Work on the Tempest Mk.IV variant was abandoned without any prototype being flown at all. The Tempest Mk.II, which was subject to repeated delays due to its Centaurus powerplant, was persisted with, but would not reach production in time to see service during the Second World War. Continual problems with the Sabre IV meant that only the single Tempest Mk.I (HM599) was built; consequently, Hawker proceeded to take the Sabre II-equipped "Tempest V" into production instead.
In August 1942, even before the first flight of the prototype Tempest V had been conducted, a production order for 400 Tempests was placed by the Air Ministry. This order was split, with the initial batch of 100 being Tempest V "Series I"s, powered by the 2,235 hp (1,491 kW) Sabre IIA series engine, which had the distinctive chin radiator, while the rest were to have been produced as the Tempest I, equipped with the Sabre IV and leading-edge radiators. These 300 Tempest Is were intended to replace an order for a similar quantity of Typhoons for the Gloster Aircraft Company.[nb 5] As it transpired, the difficulties with the Sabre IV and the wing radiators led to this version never reaching production, the corresponding order was switched to 300 Tempest V "Series 2"s instead.[nb 6]
During early 1943, a production line for the Tempest Mk. V was established in Hawker's Langley facility, alongside the existing manufacturing line for the Hawker Hurricane. Production was initially slow, claimed to be due to issues encountered with the rear spar. On 21 June 1943, the first production Tempest V, JN729, rolled off the production line and its maiden flight was conducted by test pilot Bill Humble. Several early production aircraft were used for experimental purposes; a number of these underwent extensive service trials at Boscombe Down including clearances to be fitted with external stores, including 500 lb (227 kg) and 1,000 lb (454 kg) bombs and 3 in (76.2 mm) RP-3 rockets, although few Tempest Vs deployed such ordnance operationally during the War. On 8 April 1944, the Tempest V attained general clearance.
During production of the first batch of 100 Tempest V "Series Is", distinguishable by their serial number prefix JNxxx, several improvements were progressively introduced and were used from the outset on all succeeding Tempest V "Series 2s", with serial number prefixes EJ, NV and SN. The fuselage/empennage joint originally featured 20 external reinforcing "fishplates", similar to those fitted to the Typhoon, but it was not long before the rear fuselage was strengthened and, with the fishplates no longer being needed, the rear fuselage became detachable. The first series of Tempest Vs used a built-up rear spar pick-up/bulkhead assembly (just behind the cockpit) which was adapted from the Typhoon. Small blisters on the upper rear wing root fairing covered the securing bolts. This was later changed to a new forged, lightweight assembly which connected to new spar booms: the upper wing root blisters were replaced by small "teardrop" fairings under the wings.
The first 100 Tempest Vs were fitted with 20 mm (.79 in) Hispano Mk.IIs with long barrels which projected ahead of the wing leading edges and were covered by short fairings; later production Tempest Vs switched to the short-barrelled Hispano Mk.Vs, with muzzles flush with the leading edges. Early Tempest Vs used Typhoon-style 34 by 11 inch (83.4 by 28 cm) five-spoke wheels, but most had smaller 30 by 9 inch (76.2 by 22.9 cm) four-spoke wheels. The new spar structure of the Tempest V also allowed up to 2,000 lb (907 kg) of external stores to be carried underneath the wings.
As in all mass-produced aircraft, there may have been some overlap of these features as new components became available. In mid-to-late 1944 other features were introduced to both the Typhoon and Tempest: A Rebecca transponder unit was fitted, with the associated aerial appearing under the portside centre section. A small, elongated oval static port appeared on the rear starboard fuselage, just above the red centre spot of the fuselage roundel. This was apparently used to measure the aircraft's altitude more accurately.
Unusually, in spite of the Tempest V being the RAF's best low- to medium-altitude fighter, it was not equipped with the new Mk.IIC gyroscopic gunsight (as fitted in RAF Spitfires and Mustangs from mid-1944), which would have considerably improved the chances of shooting down opposing aircraft. Tempest pilots continued to use either the Type I Mk.III reflector gunsight, which projected the sighting graticule directly onto the windscreen, or the Mk.IIL until just after the Second World War, when the gyro gunsight was introduced in Tempest IIs.
Two Tempest Vs, EJ518 and NV768, were fitted with Napier Sabre Vs and experimented with several different Napier-made annular radiators, with which they resembled Tempest IIs. This configuration proved to generate less drag than the standard "chin" radiator, contributing to an improvement in the maximum speed of some 11 to 14 mph. NV768 was later fitted with a ducted spinner, similar to that fitted to the Fw 190 V1. Another experimental Tempest V was SN354, which was fitted with a Vickers 47 mm "P" anti-tank gun, under development but never deployed, under each wing in a long "pod".[nb 7]
Tempest Mk. IIEdit
As a result of the termination of the Tornado project, Sydney Camm and his design team transferred the alternative engine proposals for the Tornado to the more advanced Tempest. Thus, it was designed from the outset to use the Bristol Centaurus 18 cylinder radial engine as an alternative to the liquid cooled engines which were also proposed. A pair of Centaurus-powered Tempest II prototypes were completed. Apart from the new engine and cowling, the Tempest II prototypes were similar to early series Tempest Vs. The Centaurus engine was closely cowled and the exhaust stacks grouped behind and to either side of the engine: to the rear were air outlets with automatic sliding "gills". The carburettor air intakes were in the inner leading edges of both wings, an oil cooler and air intake were present in the inner starboard wing. The engine installation owed much to examinations of a captured Focke-Wulf Fw 190, and was clean and effective.
On 28 June 1943, the first Tempest II, LA602, flew powered by a Centaurus IV (2,520 hp/1,879 kW) driving a four-blade propeller. LA602 initially flew with a Typhoon-type fin and rudder unit. This was followed by the second, LA607, which was completed with the enlarged dorsal fin and first flew on 18 September 1943: LA607 was assigned to engine development.[nb 8] The first major problem experienced during the first few flights was serious engine vibrations, which were cured by replacing the rigid, eight-point engine mountings with six-point rubber-packed shock mounts. In a further attempt to alleviate engine vibration, the four blade propeller was replaced with a five blade unit; eventually, a finely balanced four bladed unit was settled on. Problems were also experienced with engine overheating, poor crankshaft lubrication, exhaust malfunctions and reduction-gear seizures. Because of these problems, and because of the decision to "tropicalise" all Tempest IIs for service in the South-East Asian theatre, production was delayed.
Orders had been placed as early as September 1942 for 500 Tempest IIs to be built by Gloster but in 1943, because of priority being given to the Typhoon, a production contract of 330 Tempest IIs was allocated instead to Bristol, while Hawker were to build 1,800. This switch delayed production even more. On 4 October 1944, the first Tempest II was rolled off the line; the first six production aircraft soon joined the two prototypes for extensive trials and tests. With the end of the Second World War in sight, orders for the Tempest II were trimmed or cancelled; after 50 Tempest IIs had been built at Bristol's Banwell facility, production was stopped and shifted back to Hawker, which built a total of 402, in two production batches: 100 were built as fighters, and 302 were built as fighter-bombers (FB II) with reinforced wings and wing racks capable of carrying bombs of up to 1,000 lb.
Physically, the Tempest II was longer than the Tempest Mk.V (34 ft 5 in/10.5 m versus 33 ft 8 in/10.3 m) and 3 in (76 mm) lower. The weight of the heavier Centaurus engine (2,695 lb/1,222 kg versus 2,360 lb/1,070 kg) was offset by the absence of a heavy radiator unit, so that the Tempest II was only some 20 lb (9 kg) heavier overall. Performance was improved; maximum speed was 442 mph (711 km/h) at 15,200 ft (4,633 m) and climb rate to the same altitude took four and a half minutes compared with five minutes for the Tempest Mk. V; the service ceiling was also increased to 37,500 ft (11,430 m).
Tropicalising measures included the installation of an air filter and intake in the upper forward fuselage, just behind the engine cowling, and the replacement of the L-shaped pitot head under the outer port wing by a straight rod projecting from the port outer wing leading edge. All production aircraft were powered by a (2,590 hp/1,932 kW) Centaurus V driving a 12 ft 9 inch (3.89 m) diameter Rotol propeller. Tempest IIs produced during the war were intended for combat against Japan and would have formed part of Tiger Force, a proposed British Commonwealth long-range bomber force based on Okinawa. The Pacific War ended before they could be deployed.
Various engineering refinements that had gone into the Tempest II were incorporated into the last Tempest variant, designated as the Tempest VI. This variant was furnished with a Napier Sabre V engine with 2,340 hp (1,700 kW). The more powerful Sabre V required a bigger radiator which displaced the oil cooler and carburettor air intake from the radiator's centre; air for the carburettor was drawn through intakes on the leading edge of the inner wings, while the oil cooler was located behind the radiator. Most Tempest VIs were tropicalised, the main feature of this process being an air filter which was fitted in a fairing on the lower centre section. Other changes included the strengthening of the rear spar and the inclusion of spring tabs, which granted the variant superior handling performance.
The original Tempest V prototype, HM595, was extensively modified to serve as the Tempest VI prototype. On 9 May 1944, HM595 made its first flight after its rebuild, flown by Bill Humble. In December 1944, HM595 was dispatched to Khartoum, Egypt to conduct a series of tropical trials. During 1945, a further two Tempest V aircraft, EJ841 and JN750, were converted to the Tempest VI standard in order to participate in service trials at RAF Boscombe Down.
At one point, 250 Tempest VIs were on order for the RAF; however, the end of the war led to many aircraft programs being cut back intensively, leading to only 142 aircraft being completed. For a long time, it was thought there were Tempest VIs that had been converted for target towing purposes; however, none of the service histories of the aircraft show such conversions and no supporting photographic evidence has been found. The Tempest VI holds the distinction of being the last piston-engined fighter in operational service with the RAF, having been superseded by jet propelled aircraft.
Drawing board designsEdit
In 1944, in response to the issuing of Air Ministry Specification F.13/44, which sought a long-range fighter equipped with the Rolls Royce R.46 engine, Sydney Camm initiated work on a new design, designated as the P.1027. This was essentially a slightly enlarged Tempest which was powered by the R.46 engine, which was projected to develop around 2,500–4,000 hp (1,864–2,983 kW). This engine would have driven a set of eight-bladed contra-rotating propellers. The radiator was relocated into a ventral bath set underneath the rear fuselage and wing centre section: the wingspan was 41 ft (12.5 m) and the length was 37 ft 3 in (11.4 m).
However, work upon the P.1027 design was soon dropped in favour of concentrating upon a further developed design, designated as the P.1030. It featured wing leading edge radiators and had larger overall dimensions of 42 ft (12.8 m) wingspan and 39 ft 9 in (12.1 m) length. The top speed was expected to be in the region of 508 mph (817 km/h), with a rate of climb of 6,400 ft/min (1,951 m/min). Service ceiling was projected to be 42,000 ft (12,802 m). Work on both tenders was ultimately dropped when Camm decided to focus design efforts upon the more promising jet engine designs he was working on instead.
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The Tempest was a single engine fighter aircraft that excelled at low-level flight. In service, its primary role soon developed into performing "armed reconnaissance" operations, often deep behind enemy lines. The Tempest was particularly well suited to the role because of its high speed at low to medium altitudes, its long range when equipped with two 45-gallon drop tanks, the good firepower of the four 20mm cannon and the good pilot visibility. The three-piece windscreen and side windows of the Tempest had directly benefited from examination of captured Focke-Wulf Fw 190s, improvements included the careful design and positioning of the frame structure, blind spots being reduced to an absolute minimum. It had a bullet-resistant centre panel made up of two layers, the outer 1.5 in (38 mm) thick and the inner 0.25 in (6.5 mm).
The majority of production Tempests were powered by a single high-powered Napier Sabre II 24-cylinder engine. All versions of the Sabre drove either a four-bladed, 14 ft (4.267 m) diameter de Havilland Hydromatic or Rotol propeller. Starting with EJxxx series, on the Tempest V, both the improved Sabre IIB and IIC were used, these engines were capable of producing over 2,400 hp (1,789 kW) on emergency boost for short periods of time. Alternative engines were used on some production variants, such as the Tempest Mk II, for which a single Bristol Centaurus 18 cylinder radial engine was adopted, or the final Tempest VI, upon which a Napier Sabre V was used. Early on in development, the adoption of several other engines was proposed, some of which were tested upon multiple prototypes.
The wing of the Tempest was one of its more significant design features, having been developed from the Typhoon to use a thinner laminar flow design approach. The wing planform was of a near-elliptical shape; the aircraft's armament of four 20 mm Hispano cannons with 800 rounds of ammunition was also embedded into the wing. The ailerons were fitted with spring-loaded tabs which lightened the aerodynamic loads, making them easier for the pilot to use and dramatically improving the roll rate above 250 mph (402 km/h). The spar structure of the Tempest V also allowed the wings to carry up to 2,000 lb (907 kg) of external stores. Also developed specifically for the Tempest by Hawker was a streamlined 45 gal (205 l) "drop tank" to extend the operational radius by 500 mi (805 km) and carrier fairing; the redesigned wing incorporated the plumbing for these tanks, one to each wing.
The main undercarriage was redesigned from the Typhoon, featuring lengthened legs and a wider track (16 ft/4.9 m) to improve stability at the high landing speed of 110 mph (177 km/h), and to allow tip clearance for a new de Havilland 14 ft (4.26 m) diameter four-blade propeller. The main undercarriage units were Dowty levered suspension units incorporating trunnions which shortened the legs as they retracted. The retractable tailwheel was fully enclosed by small doors and could be fitted with either a plain Dunlop manufactured tyre, or a Dunlop-Marstrand "twin-contact" anti-shimmy tyre.
During development, Camm and the Hawker design team had placed a high priority on making the Tempest easily accessible to both air and ground crews; to this end, the forward fuselage and cockpit areas of the earlier Hurricane and the Tempest and Typhoon families were covered by large removable panels providing access to as many components as possible, including flight controls and engine accessories. Both upper wing roots incorporated panels of non-slip coating. For the pilot a retractable foot stirrup under the starboard root trailing edge was linked to a pair of handholds which were covered by spring-loaded flaps. Through a system of linkages, when the canopy was open the stirrup was lowered and the flaps opened, providing easy access to the cockpit; as the canopy was closed, the stirrup was raised into the fuselage and the flaps snapped shut.
By April 1944, the Tempest V had attained general acceptance and was in the hands of operational squadrons; 3 Squadron was the first to be fully equipped, closely followed by 486 (NZ) Squadron (the only Article XV unit to be equipped with the Tempest during the Second World War), replacing their previous Typhoons. A third unit—56 Squadron—initially kept its Typhoons and was then temporarily equipped with Spitfire IXs until sufficient supplies of Tempests were available.[nb 9] By the end of April 1944, these units were based at RAF Newchurch, a new "Advanced Landing Ground" (ALG), where they formed 150 Wing, commanded by Wing Commander Roland Beamont. The new Wing was part of the Second Tactical Air Force (2nd TAF).
Most of the operations carried out by 150 Wing comprised high-altitude fighter sweeps, offensive operations known as "Rangers", as well as reconnaissance missions. Prior to the Normandy landings, Tempests would routinely conduct long-range sorties inside enemy territory and penetrate into Northern France and the Low Countries, using a combination of cannons and bombs to attack airfields, radar installations, ground vehicles, coastal shipping and the launch sites for the German V-1 flying bombs. The build-up of Tempest-equipped squadrons was increased rapidly, in part due to factors such as the V-1 threat, although a labour strike in Hawker's assembly shop adversely affected this rate; by September 1944, a total of five frontline Tempest squadrons which comprised 114 aircraft were in operation.
In June 1944, the first of the V-1s were launched against London; the excellent low-altitude performance of the Tempest made it one of the preferred tools for handling the small fast-flying unmanned missiles. 150 Wing was transferred back to the RAF Fighter Command; the Tempest squadrons soon racked up a considerable percentage of the total RAF kills of the flying bombs (638 of a total of 1,846 destroyed by aircraft). Using external drop tanks, the Tempest was able to maintain standing patrols of 4.5 hours off the south coast of England in the approach paths of the V-1s. Guided by close instructions from coastal radar installation, Tempests would be positioned ready for a typical pursuit and would either use cannon fire or nudge the V-1 with the aircraft itself to destroy it.
In September 1944, Tempest units, based at forward airfields in England, supported Operation Market Garden, the airborne attempt to seize a bridgehead over the Rhine. On 21 September 1944, as the V-1 threat had receded, the Tempest squadrons were redeployed to the 2nd TAF, effectively trading places with the Mustang III squadrons of 122 Wing, which became part of the Fighter Command units deployed on bomber escort duties. 122 Wing now consisted of 3 Sqn., 56 Sqn., 80 Sqn., 274 Sqn. (to March 1945), and 486(NZ)Sqn. From 1 October 1944 122 Wing was based at B.80 Volkel Air Base near Uden, in the Netherlands. During the early phase of operations, the Tempest regularly emerged victorious and proved to be a difficult opponent for the Luftwaffe's Bf 109G and Fw 190 fighters to counter.
Armed reconnaissance missions were usually flown by two sections (eight aircraft), flying in finger-four formations, which would cross the front lines at altitudes of 7,000 to 8,000 feet: once the Tempests reached their allocated target area the lead section dropped to 4,000 feet or lower to search for targets to strafe, while the other section flew cover 1,000 feet higher and down sun. After the first section had carried out several attacks, it swapped places with the second section and the attacks continued until all ammunition had been exhausted, after which the Tempests would return to base at 8,000 ft. As many of the more profitable targets were usually some 250 miles from base, the Tempests typically carried two 45-gallon drop tanks which were turned on soon after takeoff. Although there were fears that the empty tanks would explode if hit by flak, the threat never eventuated and, due to the tanks being often difficult to jettison, they were routinely carried throughout an operation with little effect on performance, reducing maximum speed by 5 to 10 mph and range by 2 per cent.
Between October and December 1944, the Tempest was practically withdrawn from combat operations for overhaul work, as well as to allow operational pilots to train newcomers. The overhaul process involved the replacement or major servicing of their engines and the withdrawal of the limited number of aircraft which were equipped with spring-tabs; these increased manoeuvrability so much that there was a risk of damaging the airframe. In December 1944, upon the Tempest's reentry into service, the type had the twin tasks of the systematic destruction of the North German rail network along with all related targets of opportunity, and the maintenance of air supremacy within the North German theatre, searching for and destroying any high performance fighter or bomber aircraft of the Luftwaffe, whether in the air or on the ground.
In December 1944, a total of 52 German fighters were downed, 89 trains and countless military vehicles were destroyed, for the loss of 20 Tempests. Following the Luftwaffe's Operation Bodenplatte of 1 January 1945, 122 Wing bore the brunt of low- to medium-altitude fighter operations for the Second Tactical Air Force, which had fortuitously escaped being a victim of the extensive Bodenplatte raid, and had contributed to efforts to intercept the raiders. During this time, Spitfire XIVs of 125 and 126 Wings often provided medium- to high-altitude cover for the Tempests, which came under intense pressure, the wing losing 47 pilots in January. In February 1945, 33 and 222 Sqns. of 135 Wing converted from Spitfire Mk IXs and, in March, were joined by 274 Sqn. 135 Wing was based at B.77 Gilze-Rijen airfield in the Netherlands. The intensity of operations persisted throughout the remainder of the war.
Flying a Tempest, French ace Pierre Clostermann claimed the first Allied combat encounter with a Dornier 335 in April 1945. In his book The Big Show (pp. 273–274) he describes leading a flight of four Hawker Tempests from No. 3 Squadron RAF over northern Germany, when he intercepted a lone Do 335 flying at maximum speed at treetop level. Detecting the British aircraft, the German pilot reversed course to evade. Despite the Tempests' considerable low altitude speed, the Royal Air Force fighters were not able to catch up or even get into firing position.
During 1945, a noteworthy accomplishment of the Tempest was the scoring of a number of kills against the new German jets, including the Messerschmitt Me 262. Hubert Lange, a Me 262 pilot, said: "the Messerschmitt Me 262's most dangerous opponent was the British Hawker Tempest — extremely fast at low altitudes, highly manoeuvrable and heavily armed."
Some Me 262s were destroyed using a tactic known to 135 Wing as the "Rat Scramble"; Tempests on immediate alert took off when an Me 262 was reported to be airborne. They did not directly intercept the jet, but instead flew towards the Me 262 and Ar 234 base at Rheine-Hopsten.[nb 10] The aim was to attack jets on their landing approach, when they were at their most vulnerable, travelling slowly, with flaps down and incapable of rapid acceleration. The Germans responded by creating a "flak lane" of over 150 of the Flakvierling "quadmount" 20 mm (.79 in) AA batteries at Rheine-Hopsten, to protect the approaches. [nb 11] After seven Tempests were lost to anti-aircraft fire at Rheine-Hopsten in a single week, the "Rat Scramble" was discontinued. For a while, in March 1945, a strict "No, repeat, No ground attacks" policy was imposed; this only applied for a few days.
In air-to-air combat, the Tempest units achieved an estimated air combat success ratio of 7:1, accomplishing a 6:1 ratio against single-seat enemy fighters.[nb 12] The top-scoring Tempest pilot was Squadron Leader David C. "Foobs" Fairbanks DFC, an American who joined the Royal Canadian Air Force in 1941. By mid-1944, he was flying with 274 Squadron. When he was shot down and made a POW in February 1945, he had destroyed 11 or 12 German aircraft (and one shared), to make him the highest-scoring Tempest ace.
Early flights by RAF pilots found the Tempest, unlike the Typhoon, was buffet-free up to and somewhat beyond 500 mph (800 km/h). During 1944, several veteran USAAF pilots flew the Tempest in mock combat exercises held over the south of England; the consensus from these operations was that it was roughly akin to the American Republic P-47 Thunderbolt. According to aviation author Francis K. Mason, the Tempest was commonly accepted as the best–performing RAF fighter in operational service by VE Day. Following the end of the war, the RAF decided upon the Tempest as its standard fighter, pending the introduction of newer aircraft, many of which would be developed post-war, such as the de Havilland Hornet and the de Havilland Vampire, as well as the Gloster Meteor. A number of squadrons would operate the Tempest as their final piston-engined type before converting to the new generation of jet-powered fighter aircraft that would come to dominate the next decade and beyond.
The later Tempest Mk.II was tropicalised as it had been decided that this variant would be intended for combat against Japan. The envisioned role for the type would have been as a purpose-built type which would participate in the Tiger Force, which was a proposed British Commonwealth long-range bomber force to have been stationed on Okinawa as a forward base for operations against the Japanese mainland. Before the Tempest Mk.II entered operational service, the Pacific War ended. By October 1945, a total of 320 Tempest Mk IIs had been delivered to maintenance units stationed at RAF Aston Down and RAF Kemble; these aircraft were mainly dispatched to squadrons stationed overseas in Germany and in India, along with other locations such as Hong Kong and Malaysia. On 8 June 1946, a Tempest Mk II, flown by Roland Beamont, led the flypast at the London Victory Celebrations of 1946. RAF Tempest Mk IIs saw combat use against guerrillas of the Malayan Races Liberation Army during the early stages of the Malayan Emergency.
A total of 142 Tempest Mk VI were produced, which equipped nine squadrons of the RAF, five of these being stationed in the Middle East due to its suitability for such environments. This particular variant was anticipated to have a short lifetime and their phasing out commenced in 1949. During the 1950s, the Tempest was mainly used in its final capacity as a target tug aircraft. In 1947, the RAF transferred a total of 89 Tempest FB IIs to the Indian Air Force (IAF), while another 24 were passed on to the Pakistani Air Force (PAF) in 1948. Both India and Pakistan would operate the Tempest until 1953. Several of these aircraft remain in existence, with three being restored to airworthiness in the United States and New Zealand. The restoration of an IAF Tempest Mk.II, MW376, in New Zealand was stalled due to the unexpected death of the owner in 2013, the aircraft being sold to a Canadian enthusiast; as of April 2016, MW376 was receiving extensive work at facilities in Kelowna, British Columbia, Canada. It is being restored to an operational condition.
- Typhoon Mk II : The original designation of the Hawker Tempest.
- Tempest Mk I : Prototype fitted with the Napier Sabre IV piston engine with oil coolers and radiators placed in the wing to reduce drag, one aircraft.
- Tempest F II : Single-seat fighter aircraft for the RAF, powered by a Bristol Centaurus radial piston engine, 402 built by Hawker at Langley and 50 by Bristol Aeroplane Company, Banwell.
- Tempest FB II : Single-seat fighter-bomber with underwing pylons for bombs and rockets.
- Tempest Mk III : Prototype fitted with the Rolls-Royce Griffon piston engine.
- Tempest Mk IV : Tempest Mk III prototype re-engined with a Rolls-Royce Griffon 61 piston engine.
- Tempest Mk V : Single-seat fighter, fighter-bomber aircraft, powered by the Napier Sabre II piston engine, 801 built at Langley.
- Early series Tempest Mk V : The first 100 production aircraft were fitted with four long-barrel 20 mm (.79 in) Mark II Hispano cannons and continued to use some Typhoon components.
- Mid to late series Tempest Mk V : The other 701 production aircraft were fitted with four short-barrel 20 mm Mark V Hispano cannons and other production line changes.
- Tempest TT Mk 5 : After the Second World War a number of Tempest Mk Vs were converted to serve as target tugs.
- Tempest F Mk VI : Single-seat fighter aircraft for the RAF engined with the Sabre V (2,340 hp), 142 built.
Under restoration/privately ownedEdit
- Mk.II MW404 - under restoration to fly by Chris Miller, Texas, USA
- Mk.II G-TEMT/MW763 - under restoration to fly with Weald Aviation, North Weald, UK
- Mk.II MW810 - under restoration to fly with Nelson Ezell, Texas, USA
- Mk.V N7027E/EJ693 - under restoration to fly for Kermit Weeks, USA
- Mk.V G-TMPV/JN768 - owned by Richard Grace, Halstead, UK
- Mk.II MW376 - under restoration to fly by KF Aerospace, Kelowna, B.C., Canada 
- Mk.II LA607/N607LA - Kermit Weeks, Florida, USA
- Mk.II G-PEST/MW401 - stored, Blackbushe, UK
- Mk.II MW758 - stored, Blackbushe, UK
Specifications (Tempest V)Edit
- Crew: 1
- Length: 33 ft 8 in (10.26 m)
- Tempest II: 34 ft 5 in (10.49 m)
- Wingspan: 41 ft 0 in (12.50 m)
- Height: 14 ft 10 in (4.52 m) (tail in rigging position with one propeller blade vertical) ; 16 ft 1 in (4.90 m) (tail down with one propeller blade vertical)
- Tempest II: 13 ft 6 in (4.11 m) (tail in rigging position with one propeller blade vertical) ; 14 ft 6 in (4.42 m) (tail down with one propeller blade vertical)
- Wing area: 302 sq ft (28.1 m2)
- Airfoil: root:Hawker H.14/14/37.5 ; tip:Hawker H.14/10/37.5 (maximum thickness at 37.5% chord)
- Gross weight: 11,400 lb (5,171 kg) (interceptor) ; 12,500 lb (5,700 kg) (fighter-bomber: 2x 500 lb (230 kg) bombs) ; 13,500 lb (6,100 kg) (fighter-bomber: 2x 1,000 lb (450 kg) bombs)
- Tempest II: 11,800 lb (5,400 kg) (interceptor) ; 12,800 lb (5,800 kg) (fighter-bomber: 2x 500 lb (230 kg) bombs) ; 13,800 lb (6,300 kg) (fighter-bomber: 2x 1,000 lb (450 kg) bombs
- Tempest VI: 12,000 lb (5,400 kg) (interceptor)
- Fuel capacity: 100/130 Octane 160 imp gal (190 US gal; 730 l) internal + 90 imp gal (110 US gal; 410 l) or 180 imp gal (220 US gal; 820 l) in two auxiliary drop tanks under the wings
- Oil tank capacity: 16 imp gal (19 US gal; 73 l)
- Tempest II: 14 imp gal (17 US gal; 64 l)
- Tempest VI: 22 imp gal (26 US gal; 100 l)
- Powerplant: 1 × Napier Sabre IIB H-24 liquid-cooled sleeve-valve piston engine, 2,420 hp (1,800 kW) at + 11 lb boost for 5 minutes at sea level[nb 13] ; 2,010 hp (1,500 kW) for take-off ; 2,045 hp (1,525 kW) at 13,750 ft (4,190 m)
- Propellers: 4-bladed de Havilland Hydromatic, 14 ft (4.3 m) diameter constant-speed propeller
- Tempest II: Rotol 12 ft 9 in (3.89 m) diameter 4-bladed constant-speed propeller
- Maximum speed: 435 mph (700 km/h; 378 kn) at 17,000 ft (5,200 m) ; 390 mph (340 kn; 630 km/h) at sea level
- Tempest II: 440 mph (380 kn; 710 km/h) at 17,000 ft (5,200 m) ; 410 mph (360 kn; 660 km/h) at 29,000 ft (8,800 m) ; 400.6 mph (348.1 kn; 644.7 km/h) at sea level
- Tempest VI: 450 mph (390 kn; 720 km/h) at 14,500 ft (4,400 m) ; 425 mph (369 kn; 684 km/h) at 30,000 ft (9,100 m) ; 395 mph (343 kn; 636 km/h) at sea level
- Combat range: 420 mi (365 nmi; 676 km) Tempest II with 250 imp gal (300 US gal; 1,100 l) fuel, climb, 15 minutes combat and RTB with 20% reserve
- Service ceiling: 36,500 ft (11,100 m)
- Rate of climb: 4,700 ft/min (24 m/s)
- Time to altitude: 20,000 ft (6,100 m) in 6 minutes at combat power
- Tempest II: 20,000 ft (6,100 m) in 5 minutes at combat power
- Tempest VI: 20,000 ft (6,100 m) in 4 minutes 45 seconds at combat power
- Wing loading: 44.7 lb/sq ft (218 kg/m2) at 13,500 lb (6,100 kg)
- Power/mass: 6.7 lb/hp (4.1 kg/kW) at 13,500 lb (6,100 kg)
- Tempest II: 5.1 lb/hp (3.1 kg/kW) at 13,300 lb (6,000 kg)
- Tempest VI: 5.2 lb/hp (3.2 kg/kW) at 12,000 lb (5,400 kg)
Aircraft of comparable role, configuration and era
- Focke-Wulf Fw 190
- Lavochkin La-7
- Messerschmitt Bf 109
- Nakajima Ki-84
- North American P-51 Mustang
- Republic P-47 Thunderbolt
- Supermarine Spitfire
- Vought F4U Corsair
- Camm later remarked: "The Air Staff wouldn't buy anything that didn't look like a Spitfire."
- The renaming of the "Typhoon II" to "Tempest" was considered to be an indication of the level of changes and increasing number of refinements that had made the two aircraft more unique and distinguished from one another.
- The use of wing radiators was a point of controversy, with Air Ministry officials approaching Camm with doubts concerning its vulnerability to battle damage.
- LA610 went onto serve as the prototype for the later Hawker Fury/Sea Fury, what would be the ultimate offshoot of the Typhoon and Tempest family as well as the fastest of all Hawker-built piston-engine fighters.
- It had been intended that prefabricated Typhoon components could be reused on the Tempest, this proved to be impractical as the design production Tempest had diverged considerably from the Typhoon.
- Although JNxxx serialled Tempest Vs are called "Series 1" and later ones called "Series 2", these definitions first appeared in 1957, and there is room for doubt about them being used by Hawker during the Second World War.
- The weapon has been described, wrongly, as a 40 mm cannon in many references, including Mason 1991.
- LA607 was presented to the College of Aeronautics at Cranfield, Bedfordshire and is currently (As of 2011[update]) preserved at Fantasy of Flight at Polk city, Florida.
- According to Roland Beamont, these production delays had been caused by an industrial dispute at Langley.
- Other aircraft based there included Bf 109 and Fw 190 day fighters and Bf 110 and He 219 night fighters. The base is closer to the town of Hopsten than the city of Rheine, and is still used by the Luftwaffe.
- As well as the flak guns, there were several piston engine fighter units based in the area which were tasked to cover the jets as they were landing.
- This includes the possibility that some Tempest losses which were attributed to Flak or weather may have been due to air combat.
- Sabre IIB gave 2,420 hp (1,804 kW) at + 11 lb boost at Sea Level, 3,850 rpm.
- Mason 1967, pp. 14, 16.
- Beamont, Roland. Tempest over Europe, 1994, p. 13.
- Thomas and Shores 1988, pp. 18, 105.
- Mason 1967, pp. 3-4.
- Thomas and Shores 1988, p. 105.
- J. A. D. Ackroyd. "The Spitfire Wing Planform: A Suggestion." Journal of Aeronautical History, Paper No. 2013/02.
- .Note; both the Spitfire and the Typhoon were designed when little was known about the behaviour of air at high subsonic Mach Numbers, and of what would later become known as the Critical Mach number. The importance of this to high speed, high altitude flight would be discovered during combat in the Battle of Britain, where the Spitfire's thinner wing gave it an advantage at higher altitudes over the thicker wing-sectioned Hurricane, which was affected to a greater extent by compressibility. Fortuitously, the Spitfire had been designed with a thin wing that was subsequently discovered by the RAE to possess a high Critical Mach No.
- Mason 1967, p. 3.
- Tempest V Pilot's Notes 1944, pp. 6-7, 31.
- Bentley 1973, p. 95.
- Thomas and Shores 1988, p. 106.
- Mason 1967, p. 4.
- Mason 1967, pp. 4-6.
- Mason 1991, p. 331.
- Mason 1967, pp. 4-5.
- Mason 1967, p. 5.
- Mason 1967, p. 6.
- Mason 1991, p. 332.
- Thomas and Shores 1988, p. 107.
- Ovčáčík and Susa 2000, p. 1.
- "Discussion on first 100 Tempest V." rafcommands.com. Retrieved: 1 January 2012.
- Mason 1991, p. 333.
- Mason 1991, p. 334.
- Mason 1967, p. 7.
- Bentley 1973, pp. 92–93.
- Ovčáčík and Susa 2000, pp. 2, 4.
- Ovčáčík and Susa 2000, p. 30.
- Flight 1946, p. 91.
- Thomas and Shores 1988, p. 112.
- Williams, A. G. "The RAF'S 47 mm Class P Gun Project." quarry.nildram.co. Retrieved: 16 March 2012.
- Mason 1967, p. 13.
- Mason 1991, p. 336.
- Mason 1991, p. 337.
- Mason 1967, p. 11.
- Mason 1991, p. 339.
- Mason 1967, p. 12.
- Ovčáčík and Susa 2000, p. 2.
- Mason 1967, pp. 11-12.
- Ovčáčík and Susa 2000, pp. 2, 7–8.
- Mason 1991, p. 342.
- Mason 1991, p. 340.
- Buttler 2004, p. 30.
- Thomas and Shores 2008, p. 584.
- Ovčáčík and Susa 2000, p. 3.
- Ovčáčík and Susa 2000, p. 4.
- "Tempest MK V Performance." wwiiaircraftperformance.org. Retrieved: 10 August 2010.
- "Undercarriage blueprint." Archived 2008-03-26 at the Wayback Machine hawkertempest.se. Retrieved: 1 January 2012.
- Shores and Thomas 2008, p. 679.
- "4-Cannon Tempest Chases Nazi Robot Bomb." Popular Mechanics, February 1945.
- Mason 1967, p. 7, 10.
- Mason 1967, p. 10.
- Shores and Thomas 2008, p. 678.
- Thomas Shores and Thomas 2008, p. 585.
- Air Ministry 1944, p. 16.
- Mason 1967, pp. 10-11.
- Shores and Thomas 2008, pp. 679, 684, 686.
- "Hawker Tempest." hawkertempest.se. Retrieved: 1 January 2012.
- Clostermann 1953, p. 181.
- "Fluglehrzentrum F-4F JG 72, JBG 36." etnp.de. Retrieved: 5 January 2016, via Wayback Machine.
- "The "Westfalen-Wing" in Rheine-Hopsten." etnep.de. Retrieved: 1 January 2012.
- Thomas and Shores 1988, p. 129.
- Shores and Thomas 2008, p. 586.
- Thomas and Shores 1988, p. 193.
- "Hawker Tempest." rcaf.com. Retrieved: 3 November 2009.
- "MW404". Hawkertempest.se. Archived from the original on 12 November 2014. Retrieved 26 November 2014.
- "Hawker Tempest on the move?". Forum.keypublishing.com. Retrieved 26 November 2014.
- "MW810". Hawkertempest.se. Archived from the original on 12 November 2014. Retrieved 26 November 2014.
- "EJ693". Hawkertempest.se. Archived from the original on 12 November 2014. Retrieved 26 November 2014.
- "HAWKER TEMPEST MK V". Caa.co.uk. Retrieved 26 November 2014.
- "MW376". Hawkertempest.se.
- "LA607". Hawkertempest.se. Archived from the original on 12 November 2014. Retrieved 26 November 2014.
- "Summary". Hawkertempest.se. Retrieved 26 November 2014.
- [dead link]
- "PR536". Hawkertempest.se. Archived from the original on 12 November 2014. Retrieved 26 November 2014.
- "NV778". Hawkertempest.se. Archived from the original on 12 November 2014. Retrieved 26 November 2014.
- Bridgman, Leonard, ed. (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & Co. pp. 57c–59c.
- Bridgman 1946, pp. 126–127.
- Mason 1967, p. 16.
- Beamont, Roland. My Part of the Sky. London, UK: Patrick Stephens, 1989. ISBN 1-85260-079-9.
- Beamont, Roland. Tempest over Europe. London, UK: Airlife, 1994. ISBN 1-85310-452-3.
- Beamont, Roland. "Tempest Summer: part 1" Aeroplane Monthly, June 1992.
- Bentley, Arthur L. "Hawker Tempest Article and Drawings." Scale Models Magazine Vol. 4, No 2. February 1973. Hemel Hempstead, Hertfordshire, UK.
- Bridgman, Leonard (ed.). "The Hawker Tempest." Jane's Fighting Aircraft of World War II. London: Studio, 1946. ISBN 1-85170-493-0.
- Brown, Charles E. Camera Above the Clouds Volume 1. Shrewsbury, UK: Airlife Publishing, 1988. ISBN 0-906393-31-0.
- Buttler, Tony. British Secret Projects: Fighters and Bombers 1935–1950. Hersham, UK: Midland, 2004. ISBN 1-85780-179-2.
- Clostermann, Pierre. The Big Show. London, UK: Chatto & Windus Ltd in association with William Heinemann Ltd., 1953. No ISBN.
- Darling, Kev. Hawker Typhoon, Tempest and Sea Fury. Ramsgate, Marlborough, Wiltshire, UK: The Crowood Press Ltd., 2003. ISBN 1-86126-620-0.
- Halliday, Hugh A. Typhoon and Tempest: the Canadian Story. Charlottesville, Virginia: Howell Press, 2000. ISBN 0-921022-06-9.
- Mason, Francis K. Hawker Aircraft Since 1920 (3rd revised edition). London: Putnam, 1991. ISBN 0-85177-839-9.
- Mason, Francis K. The Hawker Typhoon and Tempest. Bourne End, Buckinghamshire, UK: Aston Publications, 1988. ISBN 0-946627-19-3.
- Mason, Francis K. The Hawker Tempest I-IV (Aircraft in Profile Number 197). Leatherhead, Surrey, UK: Profile Publications Ltd., 1967.
- "Napier Flight Development." (Article and Images)Flight No. 1961, Volume L, 25 July 1946.
- Ovčáčík, Michal and Karel Susa. Hawker Tempest: MK I, V, II, VI, TT Mks.5,6. Prague, Czech Republic: 4+ Publications, 2000. ISBN 80-902559-2-2.
- Pilot's Notes for Hawker Tempest V: Air Publication 2458c. London: Air Ministry, 1944.
- Rawlings, John D. R. Fighter Squadrons of the RAF and their Aircraft. Somerton, UK: Crécy Books, 1993. ISBN 0-947554-24-6.
- Reed, Arthur and Roland Beamont. Typhoon and Tempest at War. Shepperton, Surrey, UK: Ian Allan, 1974. ISBN 0-7110-0542-7.
- Scutts, Jerry. Typhoon/Tempest in Action (Aircraft in Action series, No. 102). Carrollton, Texas: Squadron/Signal Publications, 1990. ISBN 978-0-89747-232-6.
- Shores, Christopher. Ground Attack Aircraft of World War Two. London: Macdonald and Jane's, 1977. ISBN 0-356-08338-1.
- Tempest at War DVD, IWM Footage.
- Thomas, Chris. Typhoon and Tempest Aces of World War 2. Botley, Oxford, UK: Osprey Publishing, 1999. ISBN 1-85532-779-1.
- Thomas, Chris and Christopher Shores. The Typhoon and Tempest Story. London: Arms and Armour Press, 1988. ISBN 978-0-85368-878-5.
- Watkins, David and Phil Listemann. No. 501 (County of Gloucester) Squadron 1939–1945: Hurricane, Spitfire, Tempest. Boé Cedex, France: Graphic Sud, 2007. ISBN 978-2-9526381-3-5.
- Shores, Christopher and Chris Thomas. Second Tactical Air Force Volume One: Spartan to Normandy, June 1943 to June 1944. Hersham, Surrey, UK: Ian Allan Publishing Ltd., 2004. ISBN 1-903223-40-7.
- Shores, Christopher and Chris Thomas. Second Tactical Air Force Volume Two: Breakout to Bodenplatte, July 1944 to January 1945. Hersham, Surrey, UK: Ian Allan Publishing Ltd., 2005. ISBN 1-903223-41-5.
- Shores, Christopher and Chris Thomas. Second Tactical Air Force Volume Three: From the Rhine to Victory, January to May 1945. Hersham, Surrey, UK: Ian Allan Publishing Ltd., 2006. ISBN 1-903223-60-1.
- Shores, Christopher and Chris Thomas. Second Tactical Air Force Volume Four: Squadrons, Camouflage and Markings, Weapons and Tactics 1943–1945. Hersham, Surrey, UK: Ian Allan Publishing Ltd., 2008. ISBN 978-1-906537-01-2
|Wikimedia Commons has media related to Hawker Tempest.|
- (1944) AP 2458C.-P.N. Pilot's Notes for Tempest V Sabre IIA Engine[permanent dead link]
- Vectorsite article
- The Hawker Tempest Page
- Hawker Tempest V Performance
- U.S report on Tempest V
- Hawker Tempest profile, walkaround video, technical details for each Mk and photos
- "Spinning Intake - Ingenious Napier Development of Sabre-Tempest Annular Radiator Installation," - A 1946 Flight article on the annular radiator version of the Tempest