The Handley Page Halifax is a British Royal Air Force (RAF) four-engined heavy bomber of the Second World War. It was developed by Handley Page to the same specification as the contemporary twin-engine Avro Manchester.

The Halifax has its origins in the twin-engine HP56 proposal of the late 1930s, produced in response to the British Air Ministry's Specification P.13/36 for a capable medium bomber for "world-wide use." The HP56 was ordered as a backup to the Avro 679, both aircraft being designed to use the underperforming Rolls-Royce Vulture engine. The Handley Page design was altered at the Ministry to a four-engine arrangement powered by the Rolls-Royce Merlin engine; the rival Avro 679 was produced as the twin-engine Avro Manchester which, while regarded as unsuccessful mainly due to the Vulture engine, was a direct predecessor of the famed Avro Lancaster. Both the Lancaster and the Halifax would emerge as capable four-engined strategic bombers, thousands of which would be built and operated by the RAF and several other services during the War.

The Handley Page Halifax was a mostly orthodox design, a mid-wing monoplane with a tail unit featuring twin fins and rudders. The Halifax featured all-metal construction with a smooth, stressed skin covering the majority of the exterior surfaces; the flight control surfaces were an exception, being fabric-covered instead. The slab-sided fuselage contained a 22-foot bomb bay, which contained the majority of the Halifax's payload, while the cockpit was flush with the upper fuselage.

The Halifax was powered by four engines, two spaced evenly on each wing. Early production Halifax bombers were powered by models of the Rolls-Royce Merlin engine; later aircraft were commonly powered by the larger Bristol Hercules radial engine. To contain and attach the engines to the airframe, Handley Page developed their own design for the power egg instead of using the typical, slimmer Rolls-Royce counterpart; despite generating increased drag, this in-house design was readily adaptable to the alternative Hercules engine on later aircraft.

A total of 6,176 Halifax's and 2 prototypes were built. The Halifax served with 460,462 and 466 squadrons, RAAF.

For more information on the development, design, operational history and variants, click here.

It was part of the trio of large twin-engine bombers procured for the RAF, joining the Armstrong Whitworth Whitley and Vickers Wellington. The newest of the three medium bombers, the Hampden was often referred to by aircrews as the "Flying Suitcase" because of its cramped crew conditions. The Hampden was powered by Bristol Pegasus radial engines but a variant known as the Handley Page Hereford had in-line Napier Daggers.

The Hampden served in the early stages of the Second World War, bearing the brunt of the early bombing war over Europe, taking part in the first night raid on Berlin and the first 1,000-bomber raid on Cologne. When it became obsolete, after a period of mainly operating at night, it was retired from RAF Bomber Command service in late 1942. By 1943, the rest of the trio were being superseded by the larger four-engined heavy bombers such as the Avro Lancaster.

The Hampden Mk I had a pilot, navigator/bomb aimer, radio operator and rear gunner. Conceived as a fast, manoeuvrable "fighting bomber", the Hampden had a fixed forward-firing .303 in (7.7 mm) Browning machine gun in the upper part of the fuselage nose. To avoid the weight penalties of powered turrets, the Hampden had a curved Perspex nose fitted with a manual .303 in (7.7 mm) Vickers K machine gun and a .303 in (7.7 mm) Vickers K installation in the rear upper and lower positions. The layout was similar to the all-guns-forward cockpits introduced about the same time in Luftwaffe medium bombers, notably the Dornier Do 17. During the Norwegian Campaign, these guns proved to be thoroughly inadequate for self-defence in daylight; the single guns were replaced by twin Vickers K guns, a process led by Air Vice Marshal Arthur Harris of No. 5 Group RAF in 1940.

The Hampden had a flush-rivetted stressed skin, reinforced with a mixture of bent and extruded sections in an all-metal monocoque design. A split-assembly construction technique was employed: sections were prefabricated and then joined, to enable rapid and economic manufacture. The fuselage was in three big sections – front, centre and rear – that were built using jigs. The centre and rear sections were made of two halves, which meant that the sections could be fitted out in part under better working conditions prior to assembly. All possible assembly work was performed at the benches prior to installation upon each aircraft.

Number built:  1,430

Royal Australian Air Force
No. 455 Squadron RAAF Used between July 1941 and December 1943, Codeletters UB.

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The Handley Page HP.67 Hastings is a retired British troop-carrier and freight transport aircraft designed and manufactured by aviation company Handley Page for the Royal Air Force (RAF). Upon its introduction to service during September 1948, the Hastings was the largest transport plane ever designed for the service.

Development of the Hastings had been initiated during the Second World War in response to Air Staff Specification C.3/44, which sought a new large four-engined transport aircraft for the RAF. Early on, development of a civil-oriented derivative had been prioritised by the company, but this direction was reversed following an accident. On 7 May 1946, the first prototype conducted its maiden flight; testing revealed some unfavourable flight characteristics, which were successfully addressed via tail modifications. The type was rushed into service so that it could participate in the Berlin Airlift; reportedly, the fleet of 32 Hastings to be deployed during the RAF operation delivered a combined total of 55,000 tons (49,900 tonnes) of supplies to the city,

As the RAF's Hastings fleet expanded during the late 1940s and early 1950s, it supplemented and eventually replaced the wartime Avro York, a transport derivative of the famed Avro Lancaster bomber. RAF Transport Command operated the Hastings as the RAF's standard long-range transport; as a logistics platform, it contributed heavily during conflicts such as the Suez Crisis and the Indonesian Confrontation. A handful were also procured by the Royal New Zealand Air Force (RNZAF) to meet its transport needs. Beyond its use as a transport, several Hastings were modified to perform weather forecasting, training, and VIP duties. A civilian version of the Hastings, the Handley Page Hermes, was also produced, which only achieved limited sales. Hastings continued to be heavily used by RAF up until the late 1960s, the fleet being withdrawn in its entirety during 1977. The type was succeeded by various turboprop-powered designs, including the Bristol Britannia and the American-built Lockheed Hercules.

The Handley Page Hastings was a large purpose-built four-engine transport aircraft. It was furnished with several modern features, such as a Messier-built fully retractable undercarriage, which was operated hydraulically, and unprecedented stowage space for an RAF transport aircraft. Roughly 3,000 cubic feet of unrestricted area was used to house various cargoes or passengers. The cabin was fitted with a Plymax floor, complete with various grooves, channels, and lashing points for securing goods of varying sizes, while the walls were sound proofed and lined with plywood for increased comfort. Principal access is provided by a freight door on the port side, which incorporates a paratroop door, while a second paratroop door is present on the starboard side; on the ground, a rapidly deployable ramp suitable for road vehicles can also be used. In service, the aircraft was typically operated by a crew of five; it could accommodate either up to 30 paratroopers, 32 stretchers and 28 sitting casualties, or a maximum of 50 fully equipped troops.

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The Handley Page Heyford was a twin-engine biplane bomber designed and produced by the British aircraft manufacturer Handley Page. It holds the distinction of being the last biplane heavy bomber to be operated by the Royal Air Force (RAF).

The Heyford was developed in response to Specification B.19/27 for a new heavy night bomber. Much of the design can be attributed to the work of George Volkert, Handley Page's lead designer. Unlike the company's preceding aircraft, the Heyford comprised metal construction instead of wood; it also had an unorthodox arrangement wherein the fuselage was joined to the upper wing rather than the lower one, which gave the aircraft a relatively nose-high orientation while on the ground. Considerable revision of the proposal occurred even after its submission, which was recognised as the Air Ministry's preferred option. A sole prototype, designated Handley Page HP.38, was produced, performing its maiden flight on 12 June 1930 and commencing service trials shortly thereafter.

During November 1933, the first Heyfords entered service, being initially flown by No. 99 Squadron at RAF Upper Heyford; before the end of 1936, Bomber Command had a total of nine operational squadrons equipped with the Heyford. Despite forming a considerable portion of the RAF's bomber fleet during the mid-1930s, the Heyford had a relatively short service life as it was rapidly eclipsed by a new generation of monoplane bombers, such as the Armstrong Whitworth Whitley and the Vickers Wellington. The replacement of the type had commenced during 1937 as more capable bombers were introduced during a major rearmament push for the RAF; the Heyford was formally declared obsolete in July 1939, barely two months prior to the outbreak of the Second World War. Despite this, the type continued to be used in secondary roles, being used as glider tugs, experimental aircraft, and trainers, into the 1940s.

The Handley Page Heyford was a twin-engine biplane bomber designed for nighttime operations. It featured a relatively novel configuration in which the fuselage was attached to the upper wing – somewhat resembling the 1914-designed German Gotha G.I. This arrangement provided a favourable field of fire for its defensive weapons, which were positioned on the nose and dorsal sections, along with the ventral retractable "dustbin" turret, each of which were armed with a single .303 in (7.7 mm) Lewis light machine gun. The wings of the Heyford were equal in both span and dihedral. The lower wing featured a thickened center section to accommodate the aircraft's single bomb bay. Automated wing tip slots improved the take-off performance considerably. Propulsion consisted of a pair of Rolls-Royce Kestrel engines, which each drove a set of fixed-pitch propellers.

The Heyford featured a mixed construction; its wings were covered by fabric while the structure comprised a twin-bay metal frame, while the fuselage consisted of an aluminium monocoque forward section with a fabric-covered frame to the rear. It was operated by a crew of four, typically consisting of a pilot, a bomb aimer/navigator/gunner, a radio operator and a dorsal/ventral gunner. Open positions were provided for the pilot and both the nose and dorsal gunners. The Heyford was furnished with a fixed undercarriage that consisted of large, spat-covered wheels that were mounted at the leading edge of the lower wing. This arrangement enabled ground crews to safely attach bombs even as the engines were still running, but also had the consequence of positioning the pilot roughly 17 ft (5 m) above the ground. Another benefit of this nose-high angle was a relatively short and speedy take-off run.

Variants

H.P.38
Single prototype powered by two Rolls-Royce F.XIV engines and flown in June 1930.
H.P.50 Heyford I
Powered by 575 hp (429 kW) Rolls-Royce Kestrel III engines: 15 built, serial numbers K3489-K3902 (last aircraft built as Mk.II prototype).
H.P.50 Heyford IA
Engine support changes, power-driven generator, four-blade propellers: 23 built, serial numbers K4021-K4043.
H.P.50 Heyford II
Powered by 640 hp (480 kW) Kestrel IV engines: 16 built, serial numbers K4863-K4878.
H.P.50 Heyford III
Supercharged 695 hp (518 kW) Kestrel VI engines: 70 built in two batches, serial numbers K5180-K5199 and K6857-K6906.
For a total of 125 (including the prototype, J9130)

It was designed to take advantage of the newly developed Rolls-Royce Avon turbojet engine and the swept wing, and was the first jet-powered aircraft produced by Hawker to be procured by the RAF. On 7 September 1953, the modified first prototype broke the world air speed record for aircraft, achieving a speed of 727.63 mph (1,171.01 km/h; 632.29 kn).

The single-seat Hunter was introduced to service in 1954 as a manoeuvrable day interceptor aircraft, quickly succeeding first-generation jet fighters in RAF service such as the Gloster Meteor and the de Havilland Venom. The all-weather/night fighter role was filled by the Gloster Javelin. Successively improved variants of the type were produced, adopting increasingly more capable engine models and expanding its fuel capacity amongst other modifications being implemented. Hunters were also used by two RAF display teams: the "Black Arrows", who on one occasion looped a record-breaking 22 Hunters in formation, and later the "Blue Diamonds", who flew 16 aircraft. The Hunter was also widely exported, serving with a total of 21 overseas air forces.

The Hunter entered service with the Royal Air Force as an interceptor aircraft. It was the first jet aircraft produced by Hawker for the RAF. From the outset it was clear that the type had exceptional performance, being the first RAF aircraft capable of effectively matching the English Electric Canberra bomber. The Hunter also set numerous aviation records, including absolute speed records. The type was also lauded for its quick turnaround time – enabled by features such as its removable gun pack and pressurised fuelling system – and for its easy handling in flight.

The definitive version of the Hunter was the FGA.9, on which the majority of export versions were based. Although the Supermarine Swift had initially been politically favoured by the British Government, the Hunter proved far more successful, and had a lengthy service life with various operators, in part due to its low maintenance requirements and operating costs.

The Hunter is a conventional swept wing all-metal monoplane. The fuselage is of monocoque construction, with a removable rear section for engine maintenance. The engine is fed through triangular air intakes in the wing roots and has a single jetpipe in the rear of the fuselage. The mid-mounted wings have a leading edge sweep of 35° and slight anhedral, the tailplanes and fin are also swept. The Hunter's aerodynamic qualities were increasingly infringed upon by modifications in later production models, such as the addition of external containers to collect spent gun cartridges, underwing fuel tanks to increase range, leading edge extensions to resolve pitch control difficulties, and a large ventral air brake.

For more details of development, design, operational history and users, click here.  For detains of the large number of variants, click here.

The specifications below are for the Hunter F.6 variant.

It was overshadowed in the public consciousness by the Supermarine Spitfire's role during the Battle of Britain in 1940, but the Hurricane inflicted 60 per cent of the losses sustained by the Luftwaffe in the engagement, and fought in all the major theatres of the Second World War.

The Hurricane originated from discussions between RAF officials and aircraft designer Sir Sydney Camm about a proposed monoplane derivative of the Hawker Fury biplane in the early 1930s. Despite an institutional preference for biplanes and lack of interest from the Air Ministry, Hawker refined their monoplane proposal, incorporating several innovations which became critical to wartime fighter aircraft, including retractable landing gear and the more powerful Rolls-Royce Merlin engine. The Air Ministry ordered Hawker's Interceptor Monoplane in late 1934, and the prototype Hurricane K5083 performed its maiden flight on 6 November 1935.

In June 1936, the Hurricane went into production for the Air Ministry; it entered squadron service on 25 December 1937. Its manufacture and maintenance was eased by using conventional construction methods so that squadrons could perform many major repairs without external support. The Hurricane was rapidly procured prior to the outbreak of the Second World War in September 1939, when the RAF had 18 Hurricane-equipped squadrons in service. The aircraft was relied on to defend against German aircraft operated by the Luftwaffe, including dogfighting with Messerschmitt Bf 109s in multiple theatres of action.

The Hurricane was developed through several versions, into bomber-interceptors, fighter-bombers, and ground support aircraft as well as fighters. Versions designed for the Royal Navy known as the Sea Hurricane had modifications enabling operation from ships. Some were converted as catapult-launched convoy escorts. By the end of production in July 1944, 14,487 Hurricanes had been completed in Britain, Canada, Belgium and Yugoslavia.

For more details of the development, design, operational history and variants, click here.

It was the last propeller-driven fighter to serve with the Royal Navy, and one of the fastest production single reciprocating engine aircraft ever built. Developed during the Second World War, the Sea Fury entered service two years after the war ended. It proved to be a popular aircraft with a number of overseas militaries, and was used during the Korean War in the early 1950s, as well as against the 1961 Bay of Pigs Invasion of Cuba.

The Sea Fury's development was formally initiated in 1943 in response to a wartime requirement of the Royal Air Force (RAF), with the aircraft initially named Fury. As the Second World War drew to a close, the RAF cancelled their order for the aircraft; however, the Royal Navy saw the type as a suitable carrier aircraft to replace a range of increasingly obsolete or poorly-suited aircraft being operated by the Fleet Air Arm. Development of the Sea Fury proceeded, and the type began entering operational service in 1947.

The Sea Fury attracted international orders as both a carrier and land-based aircraft. It was operated by countries including Australia, Burma, Canada, Cuba, Egypt, West Germany, Iraq, and Pakistan. The type acquitted itself well in the Korean War, fighting effectively even against the MiG-15 jet fighter. Although the Sea Fury was retired by the majority of its military operators in the late 1950s in favour of jet-propelled aircraft, a considerable number of aircraft saw subsequent use in the civil sector, and several remain airworthy in the 21st century as heritage and racing aircraft.

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The Hawker Sea Hawk is a British single-seat jet day fighter formerly of the Fleet Air Arm (FAA), the air branch of the Royal Navy (RN), built by Hawker Aircraft and its sister company, Armstrong Whitworth Aircraft. Although its design originated from earlier Hawker piston-engined fighters, the Sea Hawk was the company's first jet aircraft.

Following acceptance in the RN, the Sea Hawk proved to be a reliable and sturdy workhorse. A considerable number were also produced for the export market and were operated from aircraft carriers in Dutch and Indian service. The last operational Sea Hawks, operated by the Indian Navy, were retired in 1983.

Towards the end of the Second World War, Hawker's design team had become increasingly interested in developing a fighter aircraft that took advantage of the newly developed jet propulsion technology. Prior to this, Hawker had been committed until late 1944 to the production and further development of its piston-powered aircraft, such as the Hurricane, Tempest and Typhoon, to meet the wartime demands for these aircraft. On 1 September 1944, the first prototype of the company's latest fighter aircraft, the Hawker Fury/Sea Fury, conducted its maiden flight; it was this aircraft that would serve as the basis for Hawker's first jet-powered aircraft.

The design team studied the potential adaption of the aircraft, having opted to use the Rolls-Royce Griffon-powered Fury prototype as the starting point. The team started with the deletion of the piston engine, with its replacement, a single Rolls-Royce Nene turbojet engine, being fitted in a mid-fuselage position, along with lateral air intakes and a tailpipe which emerged beneath the tailplane. The prospective modifications also included "stretching" the fuselage and moving the cockpit to the extreme front of the fuselage in a re-contoured nose; this design received the internal designation P.1035. Use of the Rolls-Royce Derwent engine had been studied but quickly discarded as lacking power for an aircraft of this size. In November 1944 the P.1035 design was submitted for evaluation by the Air Ministry.

In December 1944 Hawker refined the proposed design substantially. The jet exhaust was moved from beneath the tail and re-designed as two short split-lateral bifurcated exhausts (which gained the name "trouser legs"), embedded in the trailing edge of the wing root, which needed a corresponding thickening of the wing root; the air intakes were moved to the wing root leading edge, similar to the contemporary de Havilland Vampire. The shorter unusual bifurcated jet pipe reduced pressure losses in the jet pipe and had the additional advantage of freeing up space in the rear fuselage for fuel tanks, which gave the aircraft a longer range than many other early jets. The absence of wing fuel tanks also meant a thinner wing could be adopted without the penalty of reduced range; to ease manufacture, the elliptical wingform of the Fury was discarded in favour of a straight tapered wing design. The fuselage fuel tanks, being fore and aft of the engine, also provided for a stable centre of gravity during flight. The tail plane was raised to clear the jet exhausts. The Sea Hawk also featured a nose wheel undercarriage arrangement, the first for a Hawker-built aircraft. The aircraft was built to accommodate four 20mm Hispano-Suiza Mk. V cannon.

For more details of development, design, operational history and 10 variants, click here.

The Hawker Tempest is a British fighter aircraft that was primarily used in its Mk.V form by the Royal Air Force (RAF) in the later stages of the Second World War. The Tempest, originally known as the Typhoon II, was a significantly 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. Since it had diverged considerably from the Typhoon, it was renamed Tempest. The Tempest emerged as one of the most powerful fighters of World War II and at low altitude was the fastest single-engine propeller-driven aircraft of the war.

Upon entering service in 1944, the Tempest performed low-level interception, particularly against the V-1 flying bomb threat, and ground attack supporting major invasions like Operation Market Garden. Later, it successfully targeted the rail infrastructure in Germany and Luftwaffe aircraft on the ground, as well as countering similar attacks by German fighters. The Tempest was effective in the low-level interception role, including against newly developed jet-propelled aircraft like the Messerschmitt Me 262.

The further-developed Tempest 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.

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 culminated 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. Other problems had been experienced with the Typhoon, such as engine unreliability, lack of 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 was later used in the 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 m), but the wingtips were later "clipped" and the wing became shorter; 41 ft (12 m) versus 41 ft 7 in (12.67 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, but 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 use the new Mark IV version of the Napier Sabre H-block 24 cylinder engine for the Tempest, drawings of which had become available to Hawker in early 1941.

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The Hawker Tomtit is a British training biplane from the late 1920s.

The Royal Air Force in 1927 required a replacement for their current elementary trainers, the elderly Avro 504Ns. They specified that the power plant should be an Armstrong Siddeley Mongoose engine, a radial five-cylinder type, and the design should "have regards to the elimination of the Woodworking Fitter trades." In other words: the airframe, though not its covering had to be metal. This led Sydney Camm, then chief designer at Hawker to design the Tomtit, a single bay biplane whose frame was of steel and duralumin tubes. The spars were made of tubular dumbbell sections, the whole aircraft fabric covered. Automatic slats of the Handley Page type were fitted to the leading edges of the upper wing. It had the standard fixed main wheel and tail-skid undercarriage of its day. The engine was uncowled.

Instructor and trainee sat in open tandem cockpits. The latter, at the rear, was provided with the then-new blind flying panel and a cockpit hood was fitted so blind flying instruction was possible. The RAF Tomtits had 150 hp (112 kW) Mongoose IIIC motors. The prototype was first flown by George Bulman in November 1928.

Hawker also produced five civil registered Tomtits. The first two of these started with Mongoose IIIA engine and the third with an upright in-line 115 hp (86 kW) A.D.C. Cirrus Major. It was thought that this latter, lower power engine choice might appeal more to public sporting owners. Three of this group were later owned by Wolseley, who fitted them with their cowled A.R. 7 and A.R.9 radial motors.

Royal New Zealand Air Force operated 4 aircraft in the Pilot Training School. For more details of production and service, click here.

It was intended to be a medium-high altitude interceptor, as a replacement for the Hawker Hurricane but several design problems were encountered and it never completely satisfied this requirement.

The Typhoon was originally designed to mount twelve .303 inch (7.7 mm) Browning machine guns and be powered by the latest 2,000 hp engines. Its service introduction in mid-1941 was plagued with problems and for several months the aircraft faced a doubtful future. When the Luftwaffe brought the formidable Focke-Wulf Fw 190 into service in 1941, the Typhoon was the only RAF fighter capable of catching it at low altitudes; as a result it secured a new role as a low-altitude interceptor.

The Typhoon became established in roles such as night-time intruder and long-range fighter. From late 1942 the Typhoon was equipped with bombs and from late 1943 RP-3 rockets were added to its armoury. With those weapons and its four 20mm Hispano autocannons, the Typhoon became one of the Second World War's most successful ground-attack aircraft.

The basic design of the Typhoon was a combination of traditional Hawker construction (such as used in the earlier Hawker Hurricane) and more modern construction techniques; the front fuselage structure, from the engine mountings to the rear of the cockpit, was made up of bolted and welded duralumin or steel tubes covered with skin panels, while the rear fuselage was a flush-riveted, semi-monocoque structure. The forward fuselage and cockpit skinning was made up of large, removable duralumin panels, allowing easy external access to the engine and engine accessories and most of the important hydraulic and electrical equipment. Entry to the cockpit was through a door on the right side and a hinged portion of the glazed canopy. Early versions had an opaque cockpit cover behind the pilots head.

For more details of the development, design, operational history and variants of the Typhoon, click here.

The Heinkel He 162 Volksjäger (German, "People's Fighter") was a German single-engine, jet-powered fighter aircraft fielded by the Luftwaffe in World War II. Developed under the Emergency Fighter Program, it was designed and built quickly and made primarily of wood as metals were in very short supply and prioritised for other aircraft. Volksjäger was the Reich Air Ministry's official name for the government design program competition won by the He 162 design. Other names given to the plane include Salamander, which was the codename of its wing-construction program, and Spatz ("Sparrow"), which was the name given to the plane by the Heinkel aviation firm.

The aircraft was notable for its small size; although almost the same length as a Bf 109, its wing was much shorter at 7.2 metres (24 ft) vs. 9.9 metres (32 ft) for the 109. Most distinctive was its top-mounted engine, which combined with the aircraft's ground-hugging landing gear allowed the engine to be easily accessed for maintenance. This made bailing out of the aircraft without hitting the engine difficult, and the He 162 is thus also notable as the first single-engine aircraft to mount an ejection seat in an operational setting. The small size left little room for fuel, which combined with the inefficient engine resulted in very low endurance on the order of 20 minutes, and it only had room to mount two autocannons, making it quite underarmed for the era.

A series of fatal accidents during testing required a series of refinements that delayed the program, but the aircraft eventually emerged in January 1945 as an excellent light fighter. Although production lines were set up and deliveries began, the state of Germany by that time made the effort pointless. Of just less than 1,000 examples on the assembly lines, only about 120 were delivered to the airfields and most of those never flew, usually due to shortages of parts, fuel, and pilots. Small numbers were used in development squadrons and these ultimately saw combat in a few cases during April 1945, yet the He 162 also proved to be quite dangerous to its own pilots as its tiny fuel load led to a number of aircraft crashing off field, while additional losses were attributed to structural failure.

Production was still ongoing when the conflict ended in May 1945. Numerous aircraft were captured by the Allied forces along with ample supplies of parts from the production lines. Eric Brown flew one just after the war and considered it a first-rate aircraft with few vices. Several He 162s have been preserved in museum collections around the world.

for details of development and design, operational history and 10 variants, click here.

The Heinkel He 177 Greif (Griffin) was a long-range heavy bomber flown by the Luftwaffe during World War II. The introduction of the He 177 to combat operations was significantly delayed, by both problems with the development of its engines, and frequent changes to its intended role. Nevertheless, it was the only long-range, heavy bomber to become operational with the Luftwaffe during the war. The He 177 had a payload/range capability similar to that of four-engined heavy bombers used by the Allies in the European theatre.

Work on the design began in response to a 1936 requirement, known as Bomber A, issued by the RLM for a purely strategic bomber. Thus the He 177 was intended originally to be capable of a sustained bombing campaign against Soviet manufacturing capacity, deep inside Russia.

In contrast to its heavy payload and very wide, 30 metres (98 ft) planform, the specifications called for the design to have only two very powerful engines. To deliver the power required, the He 177 needed engines of at least 2,000 horsepower (1,500 kW). Engines of this type were new and unproven at the time. The Daimler-Benz DB 606 power system that was selected, in conjunction with its relatively cramped nacelles, caused cooling and maintenance problems, such that the powerplants became infamous for catching fire in flight,[3] and contributing to the He 177 gaining nicknames from Luftwaffe aircrew such as Reichsfeuerzeug ("Reich's lighter") or Luftwaffenfeuerzeug ("Air Force lighter").

The type matured into a usable design too late in the war to play an important role. It was built and used in some numbers, especially on the Eastern Front where its range was particularly useful. It is notable for its use in mass raids on Velikiye Luki in 1944, one of the late-war heavy bombing efforts by the Luftwaffe. It saw considerably less use on the Western Front, although it played a role during Operation Steinbock (the "Baby Blitz"), against the UK in 1944. A total of 1,169 were built.

For extensive further information, including design, development, operational history and 34 variants, click here.

The Heinkel He 219 Uhu ("Eagle-Owl") is a night fighter that served with the German Luftwaffe in the later stages of World War II. A relatively sophisticated design, the He 219 possessed a variety of innovations, including Lichtenstein SN-2 advanced VHF-band intercept radar, also used on the Ju 88G and Bf 110G night fighters. It was also the first operational military aircraft to be equipped with ejection seats and the first operational German World War II-era aircraft with tricycle landing gear. Had the Uhu been available in quantity, it might have had a significant effect on the strategic night bombing offensive of the Royal Air Force; however, only 294 of all models were built by the end of the war and these saw only limited service. Ernst-Wilhelm Modrow was the leading night fighter ace on the He 219. Modrow was credited with 33 of his 34 night air victories on the type.

Development and production of the He 219 was protracted and tortuous, due to political rivalries between Josef Kammhuber, commander of the German night fighter forces, Ernst Heinkel, the manufacturer and Erhard Milch, responsible for aircraft construction in the Reichsluftfahrtministerium (RLM – the German Aviation Ministry). The aircraft was also complicated and expensive to build; these factors further limited the number of aircraft produced.

When engineer Robert Lusser returned to Heinkel from Messerschmitt, he began work on a new high-speed bomber project called P.1055. This was an advanced design with a pressurized cockpit, twin ejection seats (the first to be planned for use in any combat aircraft), tricycle landing gear – featuring a nose gear that rotated its main strut through 90° during retraction (quickly orienting the nosewheel into the required horizontal position for stowage within the nose, only at the very end of the retraction cycle) to fit flat within the forward fuselage, and remotely controlled, side-mounted FDSL 131 defensive gun turrets similar to those used by the Messerschmitt Me 210. Power was to be provided by two of the potentially troublesome, dual-crankcase DB 610 "power system" engines which had started their development in June 1940, weighing on the order of about 1–1⁄2 tonnes apiece, producing (2,950 PS/2,910 hp) each, delivering excellent performance with a top speed of approximately 750 km/h (470 mph) and a 4,000 km (2,500 mi) range with a 2,000 kg (4,410 lb) bomb load.

The RLM rejected the design in August 1940 as too complex and risky. Lusser quickly offered four versions of the fighter with various wingspans and engine choices in order to balance performance and risk. At the same time, he offered the P.1056, a night fighter with four 20 mm cannon in the wings and fuselage. The RLM rejected all of these on the same grounds in 1941. Heinkel was furious and fired Lusser on the spot.

For more details on the design, development, operational history and variants, click here.

The Heinkel He 119 was an experimental single-propeller monoplane with two coupled engines, developed in Germany. A private venture by Heinkel to test radical ideas by the Günter brothers, the He 119 was originally intended to act as an unarmed reconnaissance bomber capable of eluding all fighters due to its high performance.

Design was begun in the late summer of 1936. A notable feature of the aircraft was the streamlined fuselage, most likely as an evolutionary descendant of the 1932-vintage Heinkel He 70 record-setting single-engined mailplane design, but without the He 70's protruding canopy-enclosed crew accommodation existing anywhere along the exterior. Instead, the He 119's forward fuselage featured an extensively glazed cockpit forming the nose itself, heavily framed with many diagonally braced windows immediately behind the propeller spinner's rear edge. Two of the three-man crew sat one each side of the driveshaft, which ran aft to a "power system", a coupled pair of Daimler-Benz DB 601 engines mounted above the wing center-section within the fuselage, mounted together within a common mount (the starboard component engine having a "mirror-image" centrifugal supercharger) with a common gear reduction unit fitted to the front ends of each component engine, forming a drive unit known as the DB 606, the first German aircraft to use the "high-power" powerplant system. meant to provide German aircraft with an aviation powerplant design of over-1,500 kW (2,000 PS) output capability, but weighing 1.5 tonnes apiece.

The DB 606 was installed just behind the aft cockpit wall, near the center of gravity, with an enclosed extension shaft passing through the centerline of the extensively glazed cockpit to drive a large four-blade variable-pitch airscrew in the nose. An evaporative cooling system was used on the V1, with the remaining prototypes receiving a semi-retractable radiator directly below the engine to augment cooling during take-off and climb.

Only eight prototypes were completed and the aircraft did not see production, mainly because of the shortages of DB 601 "component" engines to construct the 1,500 kg (3,300 lb) DB 606 "power systems" they formed. The first two prototypes were built as land planes, with retractable landing gear. The third prototype (V3) was constructed as a seaplane with twin floats. This was tested at the Erprobungsstelle Travemünde military seaplane test facility on the Baltic coast, and was scrapped in 1942 at Heinkel's factory airfield in the estuarine Rostock-Schmarl community, then known as Marienehe.

On 22 November 1937, the fourth prototype (V4) made a world class-record flight in which it recorded an airspeed of 505 km/h (314 mph), with a payload of 1,000 kg (2,205 lb), over a distance of 1,000 km (621 mi). The four remaining prototypes were completed during the spring and early summer of 1938, the V5 and V6 being A-series production prototypes for the reconnaissance model, and the V7 and V8 being B-series production prototypes for the bomber model.

These four aircraft were three-seaters with a defensive armament of one 7.92 mm (0.312 in) MG 15 machine gun in a dorsal position, V7 and V8 having provision for a normal bombload of three 250 kg (551 lb) bombs or maximum bombload of 1,000 kg (2,205 lb). V7 and V8 were sold to Japan in May 1940, and extensively studied; the insights thus gained were used in the design of the Yokosuka R2Y.[citation needed] The remaining prototypes served as engine test-beds, flying with various prototype versions of the DB 606 and DB 610 (twinned DB 605s) and the strictly-experimental DB 613 (twinned DB 603).

Variants

He 111U
Propaganda designation of the He 119
He 119  Specifications below)
Basic version, eight prototypes built.
He 519
1944 high-speed bomber development, designed as a private venture by Heinkel to test radical ideas by the Günter brothers, the He 519 was designed to use the 24-cylinder Daimler-Benz DB 613, but the aircraft remained a concept and was abandoned at the end of the war.

The Henschel Hs 126 was a German two-seat reconnaissance and observation aircraft of World War II that was derived from the Henschel Hs 122. The pilot was seated in a protected cockpit under the parasol wing and the gunner in an open rear cockpit. The prototype aircraft frame was that of a Hs 122A fitted with a Junkers engine. The Hs 126 was well received for its good short takeoff and low-speed characteristics which were needed at the time. It was put into service for a few years, but was soon superseded by the general-purpose, STOL Fieseler Fi 156 Storch and the medium-range Focke-Wulf Fw 189 "flying eye".

The first prototype was not entirely up to Luftwaffe standards; it was followed by two more development planes equipped with different engines. Following the third prototype, ten pre-production planes were built in 1937. The Hs 126 entered service in 1938 after operational evaluation with the Legion Condor contingent to the Spanish Civil War.

By the time the Hs 126 A-1 joined the Luftwaffe, the re-equipping of reconnaissance formations was already well advanced. By the start of World War II in September 1939, the Hs 126 served with Aufkl.Gr 10, 11, 12, 13, 14, 21, 23, 31, 32 und 41. They were used with great success in the attack on Poland where it proved itself as a reliable observation and liaison aircraft. Its use continued after the end of the Phony War in May 1940. It suffered some losses when intercepted by Allied fighter aircraft: 20 Hs 126s were lost between 10 and 21 May 1940.

Its successor, the Focke-Wulf Fw 189 entered service in 1940 but the Hs 126 remained the main short range reconnaissance aircraft until 1942. 47 squadrons equipped with Hs 126s participated in the invasion of the Soviet Union in 1941. The Hs 126 was also used in North Africa, such as with the 2./Aufklärungsgruppe (H)/14 which used the type until the end of 1942.

Late in the war, it was used in glider tug and night ground attack roles, but production of the Hs 126 ended in January 1941 and the type was retired from the front line in 1943.

The Henschel Hs 129 was a ground-attack aircraft designed and produced by the German aircraft manufacturer Henschel Flugzeugwerke AG. Fielded by the Luftwaffe during the Second World War, it saw combat in Tunisia and on the Eastern Front.

During the latter half of 1930s, influenced by the experiences of German Condor Legion during the Spanish Civil War, the Reichsluftfahrtministerium (RLM; "Reich Aviation Ministry") sought a new ground-attack aircraft. The specification required protection from ground-based small arms fire, for which Henschel's design (which was initially designated at the P 46) incorporated a steel "bathtub" with angled fuselage sides and a compact canopy that was fitted with tiny windows. A further requirement of the specification was that the aircraft be powered by engines that were not in demand for other types; accordingly, the Hs 129 was designed to be equipped with low-power German Argus As 410 engines, which were only capable of 465 PS (459 hp; 342 kW).

On 29 May 1939, the prototype Hs 129 performed its maiden flight. Early flight testing was largely unsatisfactory, the aircraft proving to be underpowered and overweight while offering poor visibility to the pilot. These problems were addressed with a new canopy with more glazing and the more powerful French Gnome-Rhône 14M engine, which could produce up to 700 PS (690 hp; 515 kW). As such, the Hs 129 A-0 was promptly succeeded by the Hs 129 A-1 and Hs 129 B-1. While Henschel faced competition to fulfil the requirement in the form of the Focke-Wulf Fw 189, the Hs 129 was both smaller and cheaper, and thus continued to hold the RLM's favour. Quantity production of the type was achieved during early 1942.

The Hs 129 was relatively effective when introduced to Luftwaffe service in April 1942. It served on the Eastern Front in a variety of frontline roles. As the conflict progressed, an emphasis on anti-tank support saw the aircraft being continually up-gunned, eventually mounting a 75 mm anti-tank cannon. Only a small number of these Hs 129 B-3 aircraft were produced to see action relatively late in the war. Production of the type peaked in 1943 and finished in September 1944 alongside Nazi Germany's declining military position, although use of the HS 129 continued into the closing months of the conflict. Despite the considerable development problems, a total of 865 units were ultimately built.

For extensive details of the development problems with the 5 variants, click here.

The Hispano HA-200 Saeta (English: Arrow) is a twin-seat jet advanced trainer designed and produced by Spanish aircraft manufacturer Hispano Aviación. It has the distinction of being the first Spanish aircraft to harness jet propulsion.

The German aircraft designer Willy Messerschmitt can be largely credited for his role in designing the HA-200, which reused a substantial portion of the earlier piston-powered HA-100 Triana. On 12 August 1955, the first prototype conducted its maiden flight. It was not until 1962 that the first production aircraft performed its first flight. That same year, deliveries of the trainer aircraft commenced to the Spanish Air Force. It would be used in this capacity by the service for multiple decades.

The HA-200 was later further developed into the Hispano Aviación Ha-220 "Super Saeta", which functioned as a dedicated ground attack platform, armed with rockets, bombs, and other munitions. The HA-220 served in the Spanish Air Force throughout the 1970s, seeing action during the Polisario uprisings against insurgents. The HA-200 was also exported, the type being produced under license by Egypt, where it was designated as the Helwan HA-200B Al-Kahira. During the 1980s, the more capable CASA C-101 was introduced to Spanish service, supplementing and eventually succeeding the older HA-200 in both trainer and light attack roles.

The HA-200 Saeta is a jet-powered trainer aircraft. In terms of its configuration, it is a low-winged monoplane, featuring all-metal construction and a retractable tricycle undercarriage arrangement. Structurally, it was relatively conventional for the era, using semi-monocoque lightweight alloy construction. The cockpit of the HA-200 accommodated a crew of two in a tandem seating configuration; however, the ground-attack orientated HA-220 was furnished with a single-seat cockpit instead. For greater crew comfort, this cockpit was pressurised, the HA-200 being the first Spanish aircraft to possess this facility.

The HA-200's propulsion consisted of a pair of Turbomeca Marboré turbojet engines, which were installed in a side-by-side arrangement inside the forward fuselage and mounted on a stressed-skin structure that forms the outer surface of the fuselage's underside. Air was fed to the engines via a large intake on the front of the nose; this particular intake arrangement has been described as being unique amongst jet aircraft. The engine's exhaust nozzles were located upon the lower fuselage, just aft of the trailing edge of the wing. A maximum of 261 gallons of fuel could be carried across a pair of fuselage tanks, two wing tanks and two permanently-attached tip tanks; provisions were made for jettisoning fuel in emergency situations. For weapons training purposes, the HA-200 featured provisions for the carriage of armaments.

For more details of development, operational history and 10 varients, click here.

The Ilyushin Il-10 (Cyrillic Илью́шин Ил-10, NATO reporting name: "Beast") was a Soviet ground attack aircraft developed at the end of World War II by the Ilyushin construction bureau. It was also license-built in Czechoslovakia by Avia as the Avia B-33.

In 1943, Ilyushin started work on a new aircraft, Il-1, which was to be a 1- or 2-seat heavily armoured fighter-interceptor, meant mainly for fighting enemy bombers and transports. The Il-1 was similar to the Il-2 design, but was more modern, compact, and powered with a new Mikulin engine: the AM-42. But the VVS gave up the idea of heavy armoured fighters, due to their low speed, which was not enough to intercept modern bombers. As a result, Ilyushin decided to turn the Il-1 into a two-seat ground attack plane, with the designation changed to Il-10 in early 1944 (odd numbers were reserved for fighters).

At that time, Ilyushin also finished a prototype of a heavier ground attack plane, the Il-8, using the same engine, and more closely derived from the Il-2. It carried a higher payload (1,000 kg/2,204 lb), but had lower performance than the Il-10. Both types first flew in April 1944, the Il-10 proving greatly superior to the Il-8, which had poor handling. The Il-10 successfully passed trials in early June 1944.

The airframe was a one engine two-seat monoplane, with a metal-covered frame. It was highly armoured. The front part of the fuselage, with the cockpit, was a shell of armour plates 4–8 mm thick; the thickest, 8 mm, were under the engine, there was no armour above the engine. The front windshield was made of armour glass 64 mm (2.5 in) thick. Also armoured were: the roof above the pilot, side window frames in the pilot's cab, the wall between crew seats, and the rear wall behind the cab. Total armour weight was 994 kg, including its attachment. The wing consisted of a central section, with two bomb bays, and two detachable outer panels. The undercarriage was retractable. The main wheels folded to the rear after rotating by 86°.

Number built    6,166 (4,966 Il-10 + 1,200 B-33)

For more details of development, design, operational history and variants, click here.

The Ilyushin Il-2 (Cyrillic: Илью́шин Ил-2) Shturmovik (Cyrillic: Штурмови́к, Shturmovík) is a ground-attack aircraft produced by the Soviet Union in large numbers during the Second World War. The Il-2 was never given an official name and 'shturmovik' is the generic Russian word meaning ground attack aircraft. The word also appears in Western sources as Stormovik and Sturmovik, neither of which give correct pronunciation in English.

The Il-2 is a single-engine, propeller-driven, low-wing monoplane of mixed construction with a crew of two (one in early versions), specially designed for assault operations. Its most notable feature was the inclusion of armor in an airframe load-bearing scheme. Armor plates replaced the frame and paneling throughout the nacelle and middle part of the fuselage, and an armored hull made of riveted homogeneous armor steel AB-1 (AB-2) secured the aircraft's engine, cockpit, water and oil radiators, and fuel tanks.

In early 1941, the Il-2 was ordered into production at four factories, and was eventually produced in greater numbers than any other military aircraft in aviation history, but by the time Nazi Germany invaded the Soviet Union on 22 June 1941, only State Aviation Factory 18 at Voronezh and Factory 381 at Leningrad had commenced production, with 249 having been built by the time of the German attack.

For more details on development, operational history and 12 variants, click here.

The Ilyushin Il-28 (Russian: Илью́шин Ил-28; NATO reporting name: Beagle) is a jet bomber of the immediate postwar period that was originally manufactured for the Soviet Air Forces. It was the Soviet Union's first such aircraft to enter large-scale production. It was also licence-built in China as the Harbin H-5. Total production in the USSR was 6,316 aircraft, and over 319 H-5s were built. Only 187 examples of the HJ-5 training variant were manufactured. In the 1990s hundreds remained in service with various air forces over 50 years after the Il-28 first appeared. The only H-5s in service currently are approximately 80 aircraft which operate with the Korean People's Air Force. The Il-28 has the USAF/DoD reporting name "Type 27" and NATO reporting name "Beagle", while the Il-28U trainer variant has the USAF/DoD reporting name "Type 30" and NATO reporting name Mascot.

After a number of attempts at a four-engined bomber (the Lyulka TR-1 powered Ilyushin Il-22 and the unbuilt Rolls-Royce Derwent powered Ilyushin Il-24), the Ilyushin Design Bureau began development of a new jet-powered tactical bomber in late 1947. Western Intelligence focused on the four-engine developments while the twin-engine Ilyushin Il-28 was created to meet a requirement for a bomber to carry a 3,000 kilograms (6,600 lb) bombload at 800 kilometres per hour (500 mph). The new design took advantage of the sale of a number of Rolls-Royce Nene jet engines by Great Britain to the Soviet Union, which allowed Soviet engineers to quickly produce an unlicensed copy of the Nene, the RD-45, with Ilyushin designing the new bomber around two RD-45s.

The Il-28 was smaller than the previous designs and carried a crew of only three (pilot, navigator and gunner). It was also smaller than the competing design from the Tupolev design bureau, the three-engined (i.e. two Nenes and a Rolls-Royce Derwent) Tupolev Tu-73, which had been started long before the Ilyushin project, and flew before the design of the Il-28 was approved.

The Il-28 design was conventional in layout, with high, unswept wings and a swept horizontal tail and fin. The engines were carried in bulky nacelles slung directly under the wings. The nosewheel retracted rearwards, while the mainwheels retracted forwards into the engine nacelles. The crew of three were accommodated in separate, pressurised compartments. The navigator, who also acted as bombardier, was accommodated in the glazed nose compartment and was provided with an OPB-5 bombsight based on the American Norden bombsight of the Second World War, while the pilot sat under a sideways opening bubble canopy with an armoured windscreen. The gunner sat in a separate compartment at the rear of the fuselage, operating a power driven turret armed with two Nudelman-Suranov NS-23 23 mm cannons with 250 rounds each. In service, the turret was sometimes removed as a weight saving measure. While the pilot and navigator sat on ejector seats, the gunner had to parachute out of a hatch in the floor in the event of an emergency. Two more fixed, forward-firing 23 mm cannon with 100 rounds each were mounted under the nose and fired by the pilot, while a bomb bay was located in the fuselage, capable of holding four 100 kg (220 lb) bombs in individual containers, or single large bombs of up to 3,000 kg (6,600 lb) slung from a beam in the bomb bay.

One unusual design feature of the Il-28 was that the wings and tail were split horizontally through the centre of the wing, while the fuselage was split vertically at the centreline, allowing the separate parts to be built individually and fitted out with systems before being bolted together to complete assembly of the aircraft. This slightly increased the weight of the aircraft structure, but eased manufacture and proved to be more economical.

The first prototype, powered by two imported Nenes, made its maiden flight on 8 July 1948, with Vladimir Kokkinaki at the controls. Testing was successful, with the Il-28 demonstrating good handling and reaching a speed of 833 km/h (518 mph). It was followed on 30 December 1948 by the second prototype, with Soviet built RD-45 engines replacing the Nenes. After the completion of state tests in early 1949 the aircraft was ordered into large scale production on 14 May 1949, with the Klimov VK-1, an improved version of the RD-45 to be used in order to improve the aircraft's performance. The first pre-production aircraft with VK-1 engines flew on 8 August 1949, and featured reshaped engine nacelles to reduce drag, while the radome for the navigation radar was moved from the rear fuselage to just aft of the nosewheel.

Full production in three factories started in September 1949, with service deliveries starting in early 1950, allowing 25 Il-28s to be displayed at the Moscow May Day parade of 1950 (as ordered by Joseph Stalin when it was ordered into production in 1949). The Il-28 soon became the standard tactical bomber in the Soviet forces and was widely exported.

For operational history and Soviet, Czechoslovak and Chinese variants, click here.

The Junkers G 31 was an advanced tri-motor airliner produced in small numbers in Germany in the 1920s. Like other Junkers types, it was an all-metal, low-wing cantilever monoplane. In the mid-1920s, the all-metal construction and an aerodynamically 'clean' configuration were remarkable.

Professor Junkers wanted to follow up on the commercial success of the tri-motor G 24 with a new design that would be larger, more comfortable for passengers, and simpler to operate and maintain.

The G 31 was the first Luft Hansa airliner to feature a flight attendant, who served food and drinks (which were not complimentary). This earned the G 31 the nickname 'flying dining car' ('fliegender Speisewagen' in German). Because of its large fuselage it was also called the flying moving van ('fliegender Möbelwagen' in German). Behind the cockpit were compartments for a radio operator, baggage and an APU that provided compressed air for main engine starting and drove a generator for electric power. The cabin was divided into three compartments that held eleven regular passenger seats, four jumpseats for passengers, a jumpseat for the steward, and an enclosed lavatory. Instead of the passenger seats, ten beds could be made up for night flying. There was a baggage and freight hold under the cabin. The wings had trailing edge flaps that reduced the landing speed by ten percent).

Professor Junkers originally requested the G 31 have landing gear that would retract into the wings. After extensive wind tunnel experiments Ernst Zindel, the leader of the design team, persuaded Professor Junkers that the gain in speed provided by reduced air resistance, would not outweigh the increased weight, cost and complexity of either retractable landing gear or simple wheel fairings. The tailskid incorporated a roller, to avoid damage to grass airfields.

The intended powerplant was three Junkers L5 engines. When these proved too weak, it was suggested to use the Napier Lion, considered to be the best aero engine at the time ("the best engine for the best plane"). This however was too expensive, especially since it would have had to be paid for in convertible currency, not German Reichsmark. Most G 31s flew with foreign air-cooled radial engines in the 500 hp range, which were licence-built in Germany (see list of variants below).

Originally, the G 31 had been intended to equip Junkers' own airline, Junkers Luftverkehr, but this venture was merged into Deutsche Luft Hansa in 1926, and the new airline purchased only eight G 31s, beginning operations in May 1928. They were used on the long-range routes of Luft Hansa, particularly to Scandinavia. They continued in this role until 1935, when replaced by the Junkers Ju 52.

Four other G 31s were sold for freighting cargo in New Guinea. Operated by Guinea Airways, one was owned by the airline itself, while the other three were owned by the Bulolo Gold Dredging Company. Powered by Pratt & Whitney Hornets, these differed from the G 31 airliners in having open cockpits, and a large hatch in the fuselage roof to accommodate the loading of bulky cargo via crane. In one particular operation, the G 31s were used to airlift eight 3,000 tonne (3,310 ton) dredges (in parts) from Lae to Bulolo. Three of the aircraft were destroyed in a Japanese air raid on Bulolo on 21 January 1942, and the remaining aircraft was pressed into RAAF service ten days later. This machine (construction number 3010, registration VH-UOW) was seriously damaged in an accident at Laverton, Victoria on 31 October that year after it careened off the runway and collided with and destroyed the Minister for Air's car. Although judged beyond repair by the Air Force, it eventually returned to freighter use in New Guinea for some time after the war.

VH-UOW, one of three G-31's pressed into RAAF service.

The Junkers Ju 290 was a large German, four-engine long-range transport, heavy bomber and maritime patrol aircraft used by the Luftwaffe late in World War II. It was developed from an airliner.

The Junkers 290 was developed directly from the Ju 90 airliner, versions of which had been evaluated for military purposes, and was intended to replace the relatively slow Focke-Wulf Fw 200 Condor, which by 1942 was proving increasingly vulnerable when confronted with Royal Air Force aircraft. The Fw 200's airframe lacked sufficient strength for the role in any case. The Ju 290 was also intended to meet the need for large transport aircraft. A bomber version, the A-8, was planned, but never built. Design was headed by Konrad Eicholtz.

The development programme resulted in the Ju 290 V1 prototype BD+TX, which first flew on 16 July 1942. It featured a lengthened fuselage, more powerful engines, and a Trapoklappe - a hydraulically operated rear loading ramp. Both the V1 and the first eight A-1 production aircraft were unarmed transports. The need for heavy transports saw the A-1s pressed into service as soon as they were completed. Several were lost in early 1943, including one taking part in the Stalingrad Airlift, and two flying supplies to German forces in Tunisia, and arming them became a priority.

The urgent need for Ju 290s in the long-range maritime reconnaissance role was now also high priority, and resulted in the Ju 290A-2. Three A-1 aircraft were converted to A-2 specification on the assembly line. Production was slow due to the modifications necessary and the installation of strong defensive armament. The A-2 was fitted with FuG 200 Hohentwiel low-UHF band search radar and a dorsal turret fitted with a 20 mm MG 151 cannon. The Hohentwiel radar was successfully used to locate Allied convoys at ranges of up to 80 km (50 mi) from an altitude of 500 m (1,600 ft) or 100 km (62 mi) from an altitude of 1,000 m (3,300 ft). It allowed the Ju 290 to track convoys while remaining out of range of anti-aircraft fire.

On 26 November 1943, Ju 290 A-5, no. 0170, along with many other new aircraft and prototypes, was shown to Adolf Hitler at Insterburg, East Prussia. Hitler was impressed by its potential and told Göring that he wanted a Ju 290 for his personal use. A Ju 290 was not however assigned to the Fliegerstaffel des Fuehrers (FdF) until late 1944, when an A-7 was supplied, works number 0192, which had formerly been assigned to FAGr 5. Modifications were completed by February 1945 at the FdF's base at Pocking, Bavaria, a Stammkennzeichen alphabetic designation code of KR+LW being applied. Hitler's pilot, Hans Baur, tested the aircraft, but Hitler never flew in it.

The aircraft was fitted with a special passenger compartment in the front of the aircraft for Hitler, which was protected by 12 mm (.5 in) armour plate and 50 mm (2 in) bulletproof glass. A special escape hatch was fitted in the floor and a parachute was built into Hitler's seat; in an emergency it was intended that he would put on the parachute, pull a lever to open the hatch, and roll out through the opening. This arrangement was tested using life-size mannequins.

Hans Baur flew the aircraft to Munich-Riem airport on 24 March 1945, landing just as an air-raid alert was sounded. He went home after parking it in a hangar but on returning to the airport, he discovered that both hangar and aircraft had been destroyed by American bombers.

Ju 290Z Zwilling
Junkers project documents from 1942 to 1944 indicate that a Zwilling (German: 'twin') variant was proposed. It was to be composed of two Ju 290 fuselages and powered by eight BMW 9-801 engines; two mounted on each outboard wing and four on the inboard wing. It was to carry a single Messerschmitt Me 328 jet parasite fighter on top of the right fuselage. The Ju 290Z was canceled in favor of the Ju 390.

For more details of the development, operational history and variants, click here.

The only photos of the Ju 290Z Zwilling available are photos of a model.

Specifications (Ju 290 A-5)

The Junkers Ju 86 was a German monoplane bomber and civilian airliner designed in the early 1930s, and employed by various air forces on both sides during World War II. The civilian model Ju 86B could carry ten passengers. Two were delivered to Swissair and five to Deutsche Luft Hansa. In addition a single civilian Ju 86Z was delivered to Sweden's AB Aerotransport.

In 1934, a specification for a modern twin-engined aircraft, capable of operating both as a high-speed airliner for the German airline Luft Hansa and as a medium bomber for the nascent Luftwaffe, was issued to both Junkers and Heinkel. Five prototypes were ordered from each company; the Junkers Ju 86 and Heinkel He 111.

Junkers' design was a low-winged twin-engined monoplane, of all-metal stressed skin construction. Unlike most of Junkers' previous designs, it discarded the typical corrugated skinning in favour of smooth metal skinning which helped to reduce drag. The craft was fitted with a narrow track retractable-main gear conventional undercarriage with a fixed tailwheel, and twin fins and rudders. It was intended to be powered by Junkers Jumo 205 diesel engines, which although heavy, gave better fuel consumption than conventional petrol engines.

The design featured the distinctive Junkers doppelflügel control surfaces on the wing, similar to those on the Junkers Ju 52. These were hinged below the wing's trailing edge, with the outboard section on each side functioning as an aileron, and the inner section functioning as a wing flap. The bomber aircraft had a crew of four; a pilot, navigator, radio operator/bombardier and gunner. Defensive armament consisted of three machine guns, situated at the nose; at a dorsal position; and within a retractable ventral position. Bombs were carried vertically in four fuselage cells behind the cockpit. The airliner version replaced the bomb cells with seating for ten passengers, with fuel tanks being moved from the fuselage to the wings.

Jumo 205s were unavailable when the first prototype airframe was completed. Instead, the bomber-configured Ju 86ab1 was fitted with Siemens SAM 22 radial engines and flew for the first time on 4 November 1934. The second prototype, also a bomber, flew in January 1935. The third Ju 86, the first civil prototype, flew on 4 April 1935. Production of pre-series military and civil aircraft started in late 1935, with full production of the Ju 86A-1 bomber commencing in April 1936. Production quickly switched to the improved Ju 86D with a modified tail cone to improve stability.

Early use of the Jumo-powered Ju 86 bomber in the Spanish Civil War showed that it was inferior to the He 111, with the diesel engines being unsuitable for rough treatment during combat; and production plans were cut back. One Ju 86 had already been converted to use radial engines as a testbed for possible export versions, and this showed improved reliability. Production switched to a version powered by the BMW 132 engine, the Ju 86E, with production continuing until 1938.

The sudden end to production without advance warning meant that there were still enough component parts to construct a further 1,000 aircraft.[10] After the war started, the Luftflotte (Air Fleet) commanders raided their training schools for Ju 52s as transport aircraft, together with their experienced aircrew instructors. This depletion continued with the formation of special bomber crews for the invasions of Norway, the Low Countries, and Crete. This was to a severe blow to the pilot training programme, and Oberstleutnant Lt-Colonel Paul Deichmann, Chief of Staff to the Luftwaffe's Chief of Training Helmuth Wilberg suggested that Ju-86s with dual controls and instruments could be easily produced to replace the appropriated Ju 52s. However, his contention that "the need for air transport services would soon reach tremendous proportions" was simply brushed aside by Göring.

Export variants

Civil variants, introduced in 1936, were designated Ju 86Z in three different models differing in their engines. The Jumo-engined Ju 86Z-1 (corresponding to the former B-0 or C-1) was sold to Swissair (one), Airlines of Australia (one), and LAN-Chile (three). The BMW 132H-powered Ju 86Z-2 was sold to DLH (two) and the para-military Manchukuo Air Transport (five or more). The Pratt & Whitney R-1690 Hornet-engined Ju 86Z-7 was delivered to AB Aerotransport (ABA) of Sweden (one, for use as a mail carrier), Lloyd Aéreo Boliviano (three), and South African Airways - SAA - (17). The ABA aircraft was later transferred to the Swedish Air Force, with which it served, under the designation Tp 9, until 1958. South African Airways' original intention was to have its Ju 86s powered by 745 hp Rolls-Royce Kestrels. Six aircraft for SAA, flown with these engines, were refitted with Hornets before delivery, and the remainder were also Hornet-powered.

The Ju 86K was an export model, also built under license in Sweden by Saab as the B 3 with (905 hp) Bristol Mercury XIX radial engines. Several aircraft remained in service with the Swedish Air Force until 1958.  A few were converted for radio interception activities.

For details of operational history and 29 variants, click here.

Picture above courtesy Geoff Goodall Collection.