The Saab 29 Tunnan ("The Barrel"), colloquially , or The Flying Barrel in English, is an early jet-powered fighter aircraft designed and produced by the Swedish aircraft manufacturer Saab. It was the second turbojet-powered combat aircraft to be developed in Sweden, the first being the Saab 21R, and it was the first Western European fighter to be produced with a swept wing after the Second World War, only being preceded in Western Europe as a whole by the Messerschmitt Me 262 built during the conflict.Boyne 2002, p. 547."1940s." Saab, Retrieved: 27 March 2016.
Work on what would become the Tunnan commenced in late 1945. The design, internally designated R 1001, had a barrel-like fuselage due to being powered by the recently developed de Havilland Ghost turbojet engine, giving it the distinctive rotund appearance from which its name is derived. A relatively thin swept wing configuration was adopted after wartime aerodynamic research from Germany indicated its favourable high speed qualities. The Swedish Air Force placed an initial order for three prototypes under the service designation J 29 during Autumn 1946. On 1 September 1948, the first prototype performed its maiden flight; flight testing proved the aircraft to exceed performance estimates in several aspects.
During May 1951, Bråvalla Wing (F 13) received the first production aircraft. Five principal variants of the Tunnan were produced; the first model to enter service being the J 29A fighter, the more capable J 29B and J 29E fighters, and finally the afterburner-equipped J 29F fighter. A dedicated aerial reconnaissance model, the S 29C, was also produced. During the 1960s, several J 29Bs saw combat while stationed in the Republic of Congo as Sweden's contribution to a UN peacekeeping mission (ONUC). The Austrian Air Force also operated the type. In service, the J 29 proved to be relatively fast and agile. The Swedish Air Force operated the type in both fighter and fighter-bomber roles into the 1970s.
Development Sweden had fallen behind the rapid technical progress being made elsewhere, and Saab needed to catch up in terms of aerodynamics and jet propulsion.Widfeldt 1966, p. 3. Accordingly, project "JxR" was initiated in late 1945 and requirements were drawn up in October 1945.Flight 1950, p. 556. A pair of proposals were presented by the Saab design team, led by Lars Brising. The first of these, codenamed R 101, nicknamed ("the cigar") due to its shape, bore a strong resemblance to the American Lockheed P-80 Shooting Star. The second design, which was chosen, was the barrel-shaped design, codenamed R 1001, which proved to be both faster and more agile. The nickname "the barrel" evolved early from this design, but for a while it also had the nickname ("One Thousand and One Nights") after the project number 1001.
The R 1001 concept had a straight wing, but after the engineers obtained German swept wing research data, it was given a 25 degree sweep. Information on swept wings came through Switzerland and included drawings for the Messerschmitt P.1101, P.1110, P.1111 and P.1112. SAAB's project manager, Frid Wänström, collected these documents in 1945 from Messerschmitt engineers who escaped to Switzerland at the end of the War. Among them was engineer and aerodynamicist Hermann Behrbohm, who joined Saab's J 29 team. These documents clearly indicated delta and swept-wing designs "reduc[e] drag dramatically as the aircraft approached the sound barrier."Erichs et al. 1988, p. 37.
To make the wing as thin as possible, the undercarriage retracted into the fuselage, rather than the wings. Wind tunnel testing at the Swedish Royal University of Technology and by the National Aeronautical Research Institute also influenced its aerodynamics.Flight 1950, p. 557. These tests determined the required fuselage form to ensure it could attain the targeted critical Mach number, as well as supporting the use of a straight-through airflow to maximize thrust.Flight 1950, pp. 556–557. Automatically locking leading edge slots, interconnected with the flaps, were also deemed necessary for lateral stability during take-off and landing. To further verify the swept wing, a Saab Safir was modified with a full-scale wing as the Saab 201. The finalized design, incorporating the new information was drawn up in January 1946.Widfeldt 1966, pp. 4–5.
The original powerplant was to have been the de Havilland Goblin turbojet, however, in December 1945, the more powerful de Havilland Ghost became available. This was ideal as not only was the Ghost set up for a circular air intake, its diameter would fit within the planned fuselage. Following negotiations between de Havilland and Saab, the Ghost engine was selected to power the type.Widfeldt 1966, p. 4.
Despite early doubts for the supply of an equivalent to the American 75S aluminium alloy, Svenska Metallverken was able to manufacture it, although significantly larger sections were used than typical for aircraft construction.Flight 1950, pp. 557-558. The structure employed heavy frames and stressed skin to meet conflicting requirements on space, strength, rigidity and accessibility.
The Swedish Air Force requested verification of the performance and a production plan for the project in February 1946. In Autumn 1946, the Swedish Air Force formally ordered three prototypes, with the type designation J 29. Static testing of the full-scale mock-up revealed problems with pressure cabin leaks, and concerning aileron behavior. A hydraulic system was installed to solve the latter issue.Widfeldt 1966, p. 5. However, these modifications delayed the first flight until after the hoped for date of 1 August 1948.
The first flight by a Saab 29 prototype was on 1 September 1948, was made by S/L 'Bob' Moore,Flight 1950, p. 558. who was later the first managing director of Saab GB, UK. A problem with the landing gear affected the expected top speed of the aircraft. Following the flight, Moore described the aircraft as "on the ground an ugly duckling – in the air, a swift." Because of the shape of its fuselage, the Saab J 29 quickly received the nickname Flygande Tunnan ("The Flying Barrel"), or Tunnan ("The Barrel") for short. While not appreciated by SAAB, its short form was eventually adopted officially."History: Saab 29 Tunnan: JAS 29 in the Swedish Air Force." Saab. Retrieved 21 March 2015.
Four prototypes were built for the test program. The first two lacked armament, carrying heavy test equipment in their place instead. The third was armed with four cannons. Air brakes on the fuselage and on the wings behind the rear spar and both conventional and combined aileron/flap arrangements were tested. Flight tests revealed that the J 29 prototypes could exceed the maximum Mach number for which they had been designed and flight performance figures were typically in excess of predicted values.
Quantity production commenced in 1948; during May 1951, Bråvalla Wing (F 13) received the first production aircraft.
The Tunnan was produced in five main variants.
The J 29A fighter was the first model to enter service, and was followed by the J 29B and J 29E fighters, and finally the afterburner-equipped J 29F fighter, which was the final variant built. There was also a dedicated reconnaissance variant, the S 29C.Widfeldt 1966, pp. 6–12. Between 1950 and 1956, 661 Tunnans were completed, the largest production run for any Saab aircraft.
Design
The Saab 29 Tunnan was the first Swedish aircraft to be specifically designed to use jet propulsion. Sweden's first jet fighter, the Saab 21R, had been modified from the piston-engined Saab 21. It is a small, chubby aircraft with a single round air intake in the nose, with the pilot under a bubble canopy directly above the air intake duct on the upper-forward section of the fuselage. It has a very thin mid-mounted moderately swept two-spar wing which is a single structure attached to the fuselage by four bolts. The undercarriage is hydraulically operated, and was designed to be suitable for use from rough airstrips. To improve pilot survivability, the Tunnan used an ejection seat Saab developed in 1943, with an explosive jettisoning system for the canopy.
The Tunnan is powered with a single de Havilland Ghost turbojet which have a top speed in excess of , better performance than Sweden's de Havilland Vampires. The engine was bolted to the fuselage at three points and a special trolley was used to remove the engine for maintenance. The final version had an afterburner, the first successful one used with a British jet engine.
Improvements were made to the wing to incorporate a dog-tooth leading edge, raising the critical Mach number. From 1963 onwards, all frontline J 29Fs were equipped with AIM-9 Sidewinder infrared-seeking air-to-air missiles.
Operational history Sweden
The J 29 was fast and agile, and set the world speed record on a closed circuit in 1954"General Aviation World Records: Saab J 29." Fédération Aéronautique Internationale (FAI). Retrieved: 18 February 2009. at 977 km/h (607.05 mph). Two S 29C (reconnaissance variant) additionally set an international speed record of 900.6 km/h (559.4 mph) over a closed-circuit course in 1955.
The crash record in early service was poor, mainly due to the inexperience with swept-winged aircraft and the lack of a two-seat, dual control Tunnan trainer variant: this meant that Swedish fighter pilots could only be trained using two seat variants of the de Havilland Vampire (a straight-winged jet), before going solo in a Tunnan. 99 pilots were killed during military practice flights in Sweden.
In May 1967, the fighter versions of the Tunnan were retired from combat service; however, a number of aircraft were retained and reconfigured for use as countermeasures trainers and for target towing duties into the 1970s. In August 1976, the last official military flight was performed at the Swedish Air Force's 50th anniversary air show.
UN operations in the Congo
The Tunnan was the first Swedish jet aircraft to see combat. In response to an appeal by the United Nations (UN) for military support in September 1961, an initial force of five J 29Bs organized as the F 22 Wing of the Swedish Air Force, were stationed in the Republic of Congo as part of Sweden's contribution to the UN peacekeeping mission in the Congo (ONUC).Widfeldt 1966, p. 9. They were subsequently reinforced by four more J 29Bs and two S 29C photo reconnaissance Tunnans in 1962.Widfeldt 1966, p. 10. The Tunnans received UN identifying markings on their fuselages.
Most missions involved attacking ground targets with cannons and unguided rockets but no aircraft were lost in action despite heavy ground fire. The consensus of the crews and foreign observers was that the Tunnan's capabilities were exceptional."J 29 – SAAB 29 "Flygande tunnan" (1951–1976)." Avrosys. Retrieved 4 December 2010."J 29 Tunnan." Everything2. Retrieved 4 December 2010. Their secessionist adversaries used a few Fouga Magisters and other aircraft with no air combat capabilities.
Swedish pilots refused some requests for close air support to ground troops, reasoning that the risk of civilian casualties was too high. In November 1962, the Swedish air commander refused a direct order to destroy the secessionist's Fouga Magisters since they were unarmed. On the 29th of December 1963, a Saab J-29 of the 22th Squadron piloted by Ake Chritianson damaged a T-6C Texan of the Katangan Airforce with the aircraft's cannons.
The only aircraft lost was by a high-ranking officer who crashed during an aborted takeoff for a test flight. When ONUC ended in 1964, some of the Swedish aircraft were deliberately destroyed at their base, as they were no longer needed in Sweden, having been superseded by later variants, and the cost of returning them wasn't justified.
Austria