The Team

The Norwegian Air Force Historical Squadron is a non-profit organization, dedicated to keeping unique aircraft in the air. The aircraft of the Norwegian Air Force Historical Squadron have been displaying at airshows all over Europe both in a formation of two or three aircraft as well as solo displays. Besides displaying at airshows the Norwegian Air Force Historical Squadron also performs heritage flights together with the Royal Norwegian Air Force helping to promote the air force and recruit future pilots. The Norwegian Air Force Historical Squadron is based at Rygge AB, 137 Air Wing, located South of Oslo and was founded in 2008.

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The Aircraft

de Havilland Vampire FB.52

The de Havilland Vampire FB.52 is a British jet fighter that was developed and manufactured by the de Havilland Aircraft Company. It was the second jet fighter to be operated by the RAF, after the Gloster Meteor, and the first to be powered by a single jet engine. The vampire FB.52 was the export version of the FB.6 Goblin 3 powered single-seat fighter-bomber.

Development of the Vampire as an experimental aircraft began in 1941 during the Second World War, to exploit the revolutionary innovation of jet propulsion. From the company's design studies, it was decided to use a single-engine, twin-boom aircraft, powered by the Halford H.1 turbojet (later produced as the "Goblin"). Aside from its propulsion system and twin-boom configuration, it was a relatively conventional aircraft. In May 1944 it was decided to produce the aircraft as an interceptor for the Royal Air Force (RAF). In 1946 the Vampire entered operational service with the RAF, only months after the war had ended.

The Vampire quickly proved to be effective and was adopted as a replacement for wartime piston-engined fighter aircraft. During its early service, it accomplished several aviation firsts and achieved various records, such as being the first jet aircraft to cross the Atlantic Ocean. The Vampire remained in front-line RAF service until 1953 when it was progressively reassigned to various secondary roles, such as ground attack and pilot training, for which specialist variants were produced. The RAF retired the Vampire in 1966 when its final role of the advanced trainer was filled by the Folland Gnat. The Royal Navy had also adapted the type as the Sea Vampire, a navalised variant suitable for operations from aircraft carriers. It was the service's first jet fighter.

The Vampire was exported to a wide variety of nations and was operated worldwide in numerous theatres and climates. Several countries deployed the type in combat during conflicts, including the Suez Crisis, the Malayan Emergency, and the Rhodesian Bush War. By the end of production, almost 3,300 Vampires had been manufactured, a quarter of these having been manufactured under licence in several other countries. In addition, de Havilland pursued the further development of the type; major derivatives produced include the DH.115, a dedicated dual-seat trainer, and the more advanced DH.112 Venom, a refined variant oriented towards conducting ground attack and night fighter operations.

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de Havilland Vampire T.55

de Havilland Vampire T.55 was the export version of the DH 115 trainer in RAF service known at the T.11. 216, six exported to Norway and in use from 1952 to 1955.

de Havilland Vampire T.55 (LN-DHZ) was licensed built in Switzerland by F+W in Emmen in the year 1959 as serial No 990 and was also their last of 20 new Swiss build two-seaters. The aircraft was flown with the Swiss Air Force marked as Vampire U-1230 until 1990. Sold on auction in 1991 to Don Wood Source Classic Flight Bournemouth.

The aircraft was purchased from Bournemouth UK in 2005 and is now operated by the Flyvåpnets Historiske Skvadron and based at Rygge Air Base near Oslo in southern Norway.

The aircraft is now in the Royal Norwegian Air Force markings to represent Vampire PX-M, a two-seater serving with 336 squadrons in the early 50s, Norway’s first pure jet fighter squadron.

RNoAF 2-seater Vampires spent time with 336, 337 and 718 Sqn. RNoAF

No less than 804 two-seat T.11 were built for the RAF and for the Royal Navy, including well over 300 for export. Numerous others were built under license.

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SBLim-2/Mig-15UTI

The two-seat SBLim-2 (SB stands for "Szkolno Bojowy" Training-Combat) is a Lim-2 (or SBLim-1) converted to a jet trainer essentially making it a Mig-15UTI.

The Lim-2 (Lim stands for "Licencyjny Mysliwiec" licensed fighter aircraft) is a licensed built Mig-15bis single-seat fighter jet powered by a Polish-built Lis-2 engine.

The Mikoyan-Gurevich MiG-15 (NATO reporting name: Fagot) is a jet fighter aircraft developed by Mikoyan-Gurevich for the Soviet Union. The MiG-15 was one of the first successful jet fighters to incorporate swept wings to achieve high transonic speeds. In combat over Korea, it outclassed straight-winged jet day fighters, which were largely relegated to ground-attack roles, and quickly countered the similar American swept-wing North American F-86 Sabre.

When refined into the more advanced MiG-17, the basic design would again surprise the West when it proved effective against supersonic fighters such as the Republic F-105 Thunderchief and McDonnell Douglas F-4 Phantom II in the Vietnam War of the 1960s.

The MiG-15 is believed to have been one of the most produced jet aircraft with more than 13,000 manufactured. Licensed foreign production may have raised the production total to almost 18,000. The MiG-15 remains in service with the Korean People's Army Air Force as an advanced trainer.

The first turbojet fighter developed by Mikoyan-Gurevich OKB was the Mikoyan-Gurevich MiG-9, which appeared in the years immediately after World War II. It used a pair of reverse-engineered German BMW 003 engines. The MiG-9 was a troublesome design that suffered from weak, unreliable engines and control problems. Categorized as a first-generation jet fighter, it was designed with the straight-style wings common to piston-engined fighters.

The Germans had been unable to develop turbojets with thrust over 1,130 kilograms-force (11,100 N; 2,500 lbf) running at the time of the surrender in May 1945, which limited the performance of immediate Soviet postwar jet aircraft designs. They did inherit the technology of the advanced axial-compressor Junkers 012 and BMW 018 engines, in the class of the later Rolls-Royce Avon, that were some years ahead of the then-available British Rolls-Royce Nene engine. The Soviet aviation minister Mikhail Khrunichev and aircraft designer A. S. Yakovlev suggested to Premier Joseph Stalin that the USSR buy the conservative but fully developed Nene engines from Rolls-Royce (having been alerted to the fact that the U.K. Labour government wanted to improve post-war UK-Russia foreign relations) for the purpose of copying them in a minimum of time. Stalin is said to have replied, "What fool will sell us his secrets?"

However, he gave his consent to the proposal and Mikoyan, engine designer Vladimir Klimov, and others travelled to the United Kingdom to request the engines. To Stalin's amazement, the British Labour government and its Minister of Trade, Sir Stafford Cripps, were perfectly willing to provide technical information and a license to manufacture the Rolls-Royce Nene. Sample engines were purchased and delivered with blueprints. Following evaluation and adaptation to Russian conditions, the windfall technology was tooled for mass-production as the Klimov RD-45 to be incorporated into the MiG-15.

To take advantage of the new engine, the Council of Ministers ordered the Mikoyan-Gurevich OKB to build two prototypes for an advanced high-altitude daytime interceptor to defend against bombers. It was to have a top speed of 1,000 kilometres per hour (620 mph) and a range of 1,200 kilometres (750 mi).

Designers at MiG's OKB-155 started with the earlier MiG-9 jet fighter. The new fighter used Klimov's British-derived engines, swept wings, and a tailpipe going all the way back to a swept tail. The German Me 262 was the first fighter fitted with an 18.5° wing sweep, but it was introduced merely to adjust the centre of gravity of its heavy Junkers Jumo 004 pioneering axial-compressor turbojet engines. Further experience and research during World War II later established that swept wings would give better performance at transonic speeds. At the end of World War II, the Soviets seized many of the assets of Germany's aircraft industry. The MiG team studied these plans, prototypes and documents, particularly swept-wing research and designs, even going so far as to produce a flying testbed in 1945 to investigate swept-wing design concepts as the piston-engined "pusher"-layout, MiG-8 Utka (Russian for "duck", from its tail-first canard design). The swept wing later proved to have a decisive performance advantage over straight-winged jet fighters when it was introduced into combat over Korea.

The design that emerged had a mid-mounted 35-degree swept wing with a slight anhedral and a tailplane mounted up on the swept tail. Western analysts noted that it strongly resembled Kurt Tank's Focke-Wulf Ta 183, a later design than the Me 262 that never progressed beyond the design stage. While the majority of Focke-Wulf engineers (in particular, Hans Multhopp, who led the Ta 183 development team) were captured by Western armies, the Soviets did capture plans and wind-tunnel models for the Ta 183. The MiG-15 bore a much stronger likeness to the Ta 183 than the American F-86 Sabre, which also incorporated German research. The MiG-15 does bear a resemblance in layout, sharing the high tailplane and nose-mounted intake, although the aircraft are different in structure, details, and proportions. The MiG-15's design understandably shared features and some appearance commonalities with the MiG design bureau's own 1945–46 attempt at a Soviet-built version of the Messerschmitt Me 263 rocket fighter in the appearance of its fuselage. The new MiG retained the previous straight-winged MiG-9's wing and tailplane placement while the F-86 employed a more conventional low-winged design. To prevent confusion during the height of combat the US painted their aircraft with bright stripes to distinguish them.

The resulting prototypes were designated I-310. The I-310 was a swept-wing fighter with a 35-degree sweep in wings and tail, with two wing fences fitted to each wing to improve airflow over the wing. The design used a single Rolls-Royce Nene fed by a split-forward air intake. A duct carried intake air around the cockpit area and back together ahead of the engine. Its first flight was 30 December 1947, some two months after the American F-86 Sabre had first flown. It demonstrated exceptional performance, reaching 1,042 kilometres per hour (647 mph) at 3,000 metres (9,800 ft).

The Soviet Union's first swept-wing jet fighter had been the underpowered Lavochkin La-160, which was otherwise more similar to the MiG-9. The Lavochkin La-168, which reached production as the Lavochkin La-15, used the same engine as the MiG but used a shoulder-mounted wing and t-tail; it was the main competitive design. Eventually, the MiG design was favoured for mass production. Designated MiG-15, the first production example flew on 31 December 1948. It entered Soviet Air Force service in 1949 and subsequently received the NATO reporting name "Fagot". Early production examples had a tendency to roll to the left or to the right due to manufacturing variances, so aerodynamic trimmers called "nozhi" (knives) were fitted to correct the problem, the knives being adjusted by ground crews until the aircraft flew correctly.

An improved variant, the MiG-15bis ("second"), entered service in early 1950 with a Klimov VK-1 engine, another version of the Nene with improved metallurgy over the RD-45, plus minor improvements and upgrades. Visible differences were a headlight in the air intake separator and horizontal upper edge airbrakes. The 23 mm cannon were placed more closely together in their undercarriage. Some "bis" aircraft also adopted under-wing hardpoints for unguided rocket launchers or 50–250 kg (110–550 lb) bombs. Fighter-bomber modifications were dubbed "IB", "SD-21", and "SD-5". About 150 aircraft were upgraded to SD-21 specification during 1953–1954.

The MiG-15 arguably had sufficient power to dive at supersonic speeds, but the lack of an "all-flying" tail greatly diminished the pilot's ability to control the aircraft as it approached Mach 1. As a result, pilots understood they must not exceed Mach 0.92, where the flight surfaces became ineffective. Additionally, the MiG-15 tended to spin after it stalled, and often the pilot could not recover. Later MiGs incorporated all-flying tails.

The MiG-15 was originally intended to intercept American bombers like the B-29. It was even evaluated in mock air-to-air combat trials with a captured U.S. B-29, as well as the later Soviet B-29 copy, the Tupolev Tu-4. To ensure the destruction of such large bombers, the MiG-15 carried autocannons: two 23 mm with 80 rounds per gun and a single 37 mm with 40 rounds. These weapons provided tremendous punch in the interceptor role, but their limited rate of fire and relatively low velocity made it more difficult to score hits against small and manoeuvrable enemy jet fighters in air-to-air combat. The 23 mm and 37 mm also had radically different ballistics, and some United Nations pilots in Korea had the unnerving experience of 23 mm shells passing over them while the 37 mm shells flew under. The cannon was fitted into a simple pack that could be winched out of the bottom of the nose for servicing and reloading, allowing pre-prepared packs to be rapidly swapped out. (Some sources mistakenly claim the pack was added in later models.)

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Canadair CT-133 Silver Star

The Canadair CT-133 Silver Star (company model number CL-30) is the Canadian license-built version of the Lockheed T-33 subsonic jet trainer aircraft, in service from the 1950s to 2005. The Canadian version was powered by the Rolls-Royce Nene 10 turbojet, whereas the Lockheed production used the Allison J33.

The Canadair CT-133 is the result of a 1951 contract to build T-33 Shooting Star Trainers for the Royal Canadian Air Force (RCAF). The powerplant would be a Rolls-Royce Nene 10 turbojet instead of the Allison J33 used by Lockheed in the production of the original T-33. A project designation of CL-30 was given by Canadair and the name was changed to Silver Star. The appearance of the CT-133 is very distinctive due to the large fuel tanks usually carried on each wingtip. A total of 656 CT-133 aircraft were built by Canadair.

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