Museo de Cuatro Vientos, Madrid, Spain

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Seeking to improve low-speed and takeoff/landing performance of the Su-7B fighter-bomber, in 1963 the Sukhoi OKB with input from TsAGI created a variable geometry wing technology demonstrator. The Su-7IG (internal designation S-22I, NATO designation Fitter-B), converted from a production Su-7BM, had fixed inner portions of the wing with movable outer segments which could be swept to 28°, 45°, or 62°. A fixed inner wing simplified construction, allowing the manufacturer to retain the Su-7 landing gear and avoiding the need for complex pivoting underwing hardpoints, and it minimized the shift in the center of pressure relative to the center of mass with change in wing sweep. The new wing also had extensive leading-edge slats and trailing-edge flaps. Su-7IG first flew on 2 August 1966 with V. S. Ilyushin at the controls, becoming the first Soviet variable geometry aircraft. Testing revealed that takeoff and landing speeds had decreased by 50-60 km/h (27-32 kn, 31-37 mph) compared to the conventional Su-7.

The production aircraft was named Su-17 (NATO designation 'Fitter-C', factory designation S-32) and was unofficially dubbed Strizh (Стриж, martlet) in service. Aside from the new wing, it differed from its predecessor Su-7 in having a new canopy and a dorsal fuselage spine for additional fuel and avionics. Su-17 first flew on 1 July 1969 with E. K. Kukushev at the controls.A total of 2,867 Su-17 and its variants were built, of which 1,165 were exported to 15 nations worldwide.

The Fitter of the museum is a Luftwaffe (ex GDR Air Force) Sukhoi Su-22M4 Fitter, 25+18.
 

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The Mikoyan-Gurevich MiG-23 (Russian: Микоян и Гуревич МиГ-23; NATO reporting name: Flogger) is a swing-wing fighter aircraft, designed by the Mikoyan-Gurevich bureau in the Soviet Union. It is considered to belong to the Soviet "Third Generation" aircraft category along with similar-aged Russian-produced fighters like the MiG-25 "Foxbat". It was the first Soviet fighter with a look-down/shoot-down radar and beyond visual range missiles, and the first MiG production fighter plane to have intakes at the sides of the fuselage. Production started in 1970 and reached large numbers with over 5,000 aircraft built. Today the MiG-23 remains in limited service with various export customers.

The Luftwaffe (ex GDR Air Force) Mikoyan Gurevitch MiG-23ML, Flogger, 20+12, was donated to Museo del Aire at Madrid Cuatro Vientos (LECU / LEVS) by the german goverment.
 

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The Mikoyan-Gurevich MiG-21 (Russian: Микоян и Гуревич МиГ-21) (NATO reporting name "Fishbed") is a supersonic jet fighter aircraft, designed by the Mikoyan-Gurevich Design Bureau in the Soviet Union. It was popularly nicknamed "balalaika", from the aircraft's planform-view resemblance to the Russian stringed musical instrument or ołówek (English: pencil) by Polish pilots due to the shape of its fuselage. Early versions are considered second-generation jet fighters, while later versions are considered to be third-generation jet fighters. Some 50 countries over four continents have flown the MiG-21, and it still serves many nations a half-century after its maiden flight. The fighter made aviation records. At least by name, it is the most-produced supersonic jet aircraft in aviation history and the most-produced combat aircraft since the Korean War, and it had the longest production run of a combat aircraft (1959 to 1985 over all variants).

This Luftwaffe (former GDR Air Force) MiG-21SPS, 22+26 was donated to Museo del Aire where is on display. Madrid Cuatro Vientos (LECU / LEVS).
 

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he Mikoyan-Gurevich MiG-17 (Russian: Микоян и Гуревич МиГ-17) (NATO reporting name: Fresco) (China:Shenyang J-5) (Poland: PZL-Mielec Lim-6)[1] is a high-subsonic performance jet fighter aircraft produced in the USSR from 1952 and operated by numerous air forces in many variants. It is an advanced development of the very similar appearing MiG-15 of the Korean War, and was used as an effective threat against supersonic fighters of the United States in the Vietnam War. It was also briefly known as the "Type 38", by USAF designation prior to the development of NATO codes.

The Mig-17 of the museum belonged to the Bulgarian Air Force.
 

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The majority of Albatrosses were used by the U.S. Air Force, primarily by the Air Rescue Service, and initially designated as SA-16. The USAF utilized the SA-16 extensively in Korea for combat rescue, where it gained a reputation as a rugged and seaworthy craft. Later, the redesignated HU-16B (long-wing variant) Albatross was used by the U.S. Air Force's Aerospace Rescue and Recovery Service and saw extensive combat service during the Vietnam conflict.

The U.S. Navy also employed the HU-16D Albatross as a Search And Rescue aircraft from coastal naval air stations, both stateside and overseas. It was also employed as an operational support aircraft worldwide and for "skunk runs" from the former NAS Agana, Guam during the Vietnam War. Goodwill flights were also common to the surrounding Trust Territory of the Pacific Islands in the early 1970s. Open water landings and water takeoff training using JATO was also frequently conducted frequently by U.S. Navy HU-16s from locations such as NAS Agana, Guam; Naval Station Guantanamo Bay, Cuba; NAS Barbers Point, Hawaii; and NAS Pensacola, Florida, among other locations.

The HU-16 was also operated by the U.S. Coast Guard as both a coastal and long-range open ocean SAR aircraft for many years until it was supplanted by the HU-25 Guardian and HC-130 Hercules.
 

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The Saab Company was approached in 1948 to develop a turbojet-powered strike aircraft to replace a series of 1940s vintage attack, reconnaissance and night-fighter aircraft in the Flygvapnet: the Saab B 18/S 18, J 21R/A 21R and J 30 (de Havilland Mosquito). The design was initially designated the P1150.

Swedish Air Force requirements for the P1150 were demanding: the aircraft had to be able to attack anywhere along Sweden's 1,245 miles (2000 km) of coastline within one hour of launch from a central location. It had to be capable of being launched in any weather, day or night. Special attention was to be paid to integrating the electronics and weapons systems to create the equivalent of today's weapons systems approach to combat aircraft design. The aircraft was to be armed with four 20 mm cannons, rockets, bombs and/or a new anti-ship missile being developed, the Rb 04.

The design team created a sleek airframe with clean lines powered by a license-built Rolls-Royce Avon Series 100. Uniquely, the design of the swept wings was the result of an early application of computer technology. To test the 35° sweepback design, a half-scale wing was mounted on a Saab Safir, the Saab 202 Safir. The design initially featured both Fowler flaps and a leading edge slot. The slot was discarded as unnecessary after trials with the prototypes and never appeared on a production aircraft. A small batch of P1150 prototypes completed design and evaluation trials with series production of the newly renamed Saab J 32 Lansen ("Jakt" [Fighter]) beginning in 1953. There were no trainer versions, but some Lansens had rudimentary controls installed in the rear seat.

This Lansen was given to the museum by the Swedish govermente
 

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The Saab 37 Viggen (English: Thunderbolt) was a Swedish single-seat, single-engine, short-medium range fighter and attack aircraft, manufactured between 1970 and 1990. Several variants were produced to perform the roles of all-weather fighter-interceptor, ground attack and photo-reconnaissance, as well as a two-seat trainer.
 

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A trainning airplane of the "Fuerzas Aereas Republica Española" (FARE)
 

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he Morane-Saulnier G was a sport aircraft produced in France in the years before the First World War. It was a development of the racing monoplanes designed by Léon Morane and Raymond Saulnier after leaving Borel and like its predecessors, was a conventional, wire-braced, shoulder-wing design. Construction was of fabric-covered wood throughout, except for the undercarriage struts which were of steel tube.

The type was a sporting success. In April 1913, Roland Garros took second place in the inaugural Schneider Cup in a floatplane version, finishing with a time of 40 minutes 40 seconds. On 26 June, Claude Grahame-White flew another float-equipped example from Paris to London via Le Havre, Boulogne-sur-Mer, and Dover, covering some 500 km (300 miles) that day.Between 21 and 28 September the same year, two float-equipped Type Gs competed at the seaplane meeting at San Sebastián, with Lord Carbery winning the short take-off prize on one, and Edmond Audemars winning the maneuverability prize on the other. The following week, Carbery flew his Type G in the Italian Waterplane Contest from Lake Como to Pavia and back, along with two other Type Gs in the field of fifteen competitors, these flown by Garros and Morane. Garros not only won the Grand Prize in the "general class", but also the prizes for best speed (127.7 km/h, 79.8 mph) and greatest altitude (2,100 m, 6,000 ft).

In 1914, Russian manufacturer Duks arranged to build the type under licence at their Moscow factory for the Russian Army, and the same year, the Turkish military ordered 40 examples. Before these could be delivered, however, war broke out, and the aircraft were impressed into the French Army. To these, the Army soon added an order of 94 aircraft, and the British Royal Flying Corps also acquired a number, these latter machines purchased from Grahame-White, who was manufacturing the type in the UK under licence. At the outbreak of war, the type's military value was found to be wanting, and the French machines were quickly relegated to training duties. Despite this, a dedicated single-seat fighter version was built in 1915, armed with an 8 mm Hotchkiss machine gun that fired through the propeller arc, the propeller blades being protected by deflector plates. Only one or two prototypes were built, and the type never entered service.

Some Type Gs were modified by Morane-Saulnier to have their wings mounted above the fuselage, parasol-fashion, rather than at the fuselage sides. This arrangement was found to offer far better visibility for the pilot, and formed the basis for the Morane-Saulnier L. A Type G is preserved at the Museo del Aire de Cuatrovientos in Madrid.
 

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The Fokker C.I was a German reconnaissance biplane under development at the end of World War I. The design was essentially an enlarged Fokker D.VII fighter with two seats and a 138 kW (185 hp) BMW IIIa engine. The C.I was originally developed to sell to the German Army. It never saw service in World War I, but Anthony Fokker managed to smuggle parts out of Germany at the time of the Armistice. The C.III version eas a two-seat advanced trainer version of the C.I, powered by a 164 kW (220 hp) Hispano-Suiza engine.
 

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The MBB Bo 105 is a light, twin-engine, multi-purpose utility helicopter developed by Bölkow of Stuttgart, Germany. Production began under Messerschmitt-Bölkow-Blohm (MBB), which became a part of Eurocopter in 1991. Eurocopter continued to produce the Bo 105 until 2001. It was replaced in the product line by the EC 135.

The Bo 105A made its maiden flight on the 16th February 1967 at Ottobrunn in Germany with Messerschmitt-Bölkow-Blohm's test pilot, Wilfried von Engelhardt, at the controls. The German Civil Aviation Authority certified the helicopter on 13 October 1970 and production for German civil and law enforcement organizations began shortly afterwards. Further safety certification by the FAA was granted in April 1972 with United States export orders following. The Bo 105C was developed in 1972 and the German Ministry of Defence selected this model for its light observation helicopter program, purchasing 100 helicopters in 1977. A specialist anti-tank version armed with Euromissile HOT missiles and designated as the Bo 105PAH-1 was procured by the German Army around the same time, with a total of 212 eventually being delivered.

In 1976, the Bo 105CB was developed with more powerful Allison 250-C20B engines. This was further developed as the Bo 105CBS with the enlargement of the fuselage by 10 inches to meet American market demands for emergency medical service operations, with this version becoming known as the Bo 105 Twin Jet in the United States. In 1984, the Bo 105LS was developed with the enlarged fuselage of the Bo 105CBS combined with more powerful Allison 250-C28C engines to increase the maximum take-off weight.

Production ended in 2001, due to the Bo 105 being superseded by the more modern Eurocopter EC 135, after 1,406 machines had been built. The last BO105-LS was delivered in 2009 to Dam Helicopters Inc. of Nelson, BC, Canada. Being the first light twin-engined helicopter in commercial service, it gained widespread use over rural areas (police and EMS / medevac) as well as offshore.

In Spain, it has been used as an attack helicopter and also by the "Guardia Civil" (military police).
 

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The Stampe et Vertongen SV.4 (also known as the Stampe SV.4 or just Stampe) is a Belgian two-seat trainer/tourer biplane designed and built by Stampe et Vertongen. The aircraft was also built under licence in France and Algeria. The SV.4 was designed as a biplane tourer/training aircraft in the early 1930s by Stampe et Vertongen at Antwerp. The first model was the SV.4A an advanced aerobatic trainer followed by the SV.4B with redesigned wings and the 130 hp/97 kW de Havilland Gipsy Major.

Only 35 aircraft were built before the company was closed during the Second World War. After the war the successor company Stampe et Renard built a further 65 aircraft between 1948 and 1955 as trainers for the Belgian Air Force. A licenced SV.4C version was built in France by SNCAN (Société Nationale de Constructions Aéronautiques du Nord) and in Algeria by Atelier Industriel de l'Aéronautique d'Alger, the two firms completing a combined total of 940 aircraft. The postwar SV.4Cs were widely used by French military units as a primary trainer. Many also served with aero clubs in France, numbers of which were later sold secondhand to the United Kingdom and other countries.
 

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The Northrop F-5A/B Freedom Fighter and F-5E/F Tiger II are part of a family of widely used light supersonic fighter aircraft, designed and built by Northrop in the United States, beginning in 1960s. Hundreds remain in service in air forces around the world in the early 21st Century, and the type has also been the basis for a number of other aircraft.

The F-5 started life as a privately funded light fighter program by Northrop in the 1950s. The first generation F-5A Freedom Fighter entered service in the 1960s. Over 800 were produced through 1972 for U.S. allies during the Cold War. The USAF had no need for a light fighter, but it did specify a requirement for a supersonic trainer and procured about 1,200 of a derivative airframe for this purpose, the T-38 Talon.

The improved second-generation F-5E Tiger II was also primarily used by American Cold War allies and, in limited quantities, served in US military aviation as a training and aggressor aircraft; Tiger II production amounted to 1,400 of all versions, with production ending in 1987. Many F-5s continuing in service into the 1990s and 2000s have undergone a wide variety of upgrade programs to keep pace with the changing combat environment. The F-5 was also developed into a dedicated reconnaissance version, the RF-5 Tigereye.

The F-5 serves as a starting point for a series of design studies which resulted in the twin-tailed Northrop YF-17 and the F/A-18 series of carrier-based fighters. The F-20 Tigershark was an advanced version of the F-5E that did not find a market. The F-5N/F variants remain in service with the United States Navy as an adversary trainer. In Sapin they are also used as advanced trainers.

Versions:

SF-5A: Single-seat fighter version of the F-5A. Built under licence in Spain by CASA.

SRF-5A: Single-seat reconnaissance version of the RF-5A. Built under license in Spain By CASA.

SF-5B: Two-seat training version of the F-5B. Built under license in Spain by CASA.
 

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Miles' previous experience with the Southern Martlet and Metal Martlet biplanes led to the desire to build a two-seat monoplane replacement for biplanes which had virtually cornered the market. The result was the M.2 Hawk, flown in March 1933 and the forerunner of a brilliant series of Miles monoplanes. Powered originally by the 71kW Cirrus IIIA engine, later M.2c aircraft offered the 89kW de Havilland Gipsy III. Other variants included the M.2a with an enclosed cabin, M.2b single-seat long-range version with an 89kW Hermes IV engine, and the three-seat M.2d. Hawk production totalled 55.

Further development of the basic type led to the Hawk Major series (64 built), beginning with the M.2F with the 97kW de Havilland Gipsy Major engine and encompassing a whole range of variants up to the M.2T. Single-seat racing models were known as the Hawk Speed Six; three were built with 149kW Gipsy Six engines, and another somewhat smaller racing variant was the M.5 Sparrowhawk, of which five were built. The prototype survived the war and in 1953 was modified considerably by the installation of two 150kg thrust Turbomeca Palas jet engines to become the M.77 Sparrowjet with a speed of 370km/h. The final pre-war development was the Hawk Trainer, of which 25 were built, and the basic design was later developed into the M.14 Magister.
 

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The Mi-2 was produced exclusively in Poland, in the WSK "PZL-Świdnik" factory in Świdnik. Production ended in 1985 after about 7,200 were made. The first production helicopter in the Soviet Union was the Mil Mi-1, modelled along the lines of the S-51 and Bristol Sycamore and flown by Mikhail Mil's bureau in September 1948. During the 1950s it became evident, and confirmed by American and French development, that helicopters could be greatly improved with turbine engines. S. P. Isotov developed the GTD-350 engine and Mil used two of these in the far superior Mi-2. After initial development at the Mil bureau (Soviet designation V-2) this was transferred to Poland in 1964, after the first Swidnik-built example had flown. WSK-Świdnik has since delivered many hundreds, possibly one-third of them to military customers, and developed plastic rotor blades and the wide-body Mi-2M seating 10 passengers instead of eight. Most typical role kits include four stretchers, as air ambulance, or aerospraying or cropdusting device.

In Poland, there were also developed several specialized military variants, first of all support or reconnaissance ones, with 23 mm autocannon, machine guns and/or two 57 mm rocket pods, four 9K11 Malyutka anti-tank missiles or Strela-2 AA missiles.
 

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Klemm L.25, later Klemm Kl 25 was a successful German light leisure and training monoplane aircraft, developed in 1928. More than 600 aircraft were built, and manufacturing licenses were sold to the United Kingdom and the United States. With low cantilever wing, fixed landing gear, and two open cockpits, the aircraft was developed by Hanns Klemm who used his previous design, the Klemm Kl 20, as a starting point. It first flew on a 20 hp (15 kW) Mercedes engine. About thirty different versions of the Kl 25 were made, and these were equipped with engines ranging from 32 to 70 kW (43 to 94 hp). The fuselage was covered with plywood.

Depending on the model, the aircraft's weight was 620 to 720 kg (1,367 to 1,587 lb), and it had a 10.5 to 13 m (34 to 43 ft) wingspan. Take-off was achieved at only 50 km/h (31 mph) and the maximum speed was between 150 to 160 km/h (93 to 99 mph). In relation to similar aircraft of the time, assembly was very easy, and this made it a very popular aircraft. According to the sales brochures, only 25% of the engine's power was needed to keep the aircraft flying, compared to biplanes of the period, which required 50% engine power. About 600 were built in Germany between 1929 and 1936,[1] serving with various flight training organizations, on either wheels, skis, or floats. Fifteen were sold to Britain before the Second World War, being fitted with a variety of domestic engines, while twenty-eight more were built by British Klemm Aeroplane Company as the B.A. Swallow.
 

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The HS-34 was designed by the engineer D. Vicente Roa and built at the Guadalajara´s Hispano Suiza factory. It was a mixed construction airplane of steel tubes and wood, being desinged to participe in a contest of the "Aviacion Militar Española" (AME) in 1935 to acquired a basic trainning plane. The prototype was evaluated and five more examples were requested. When the Spanish Civil War broke out, the factory and the prototypes were moved to the Rabasa airfield, in Alicante, were it served as a liaison aircraft.
 

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