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Kalmar Wing
Kalmar Wing ( sv, Kalmar flygflottilj), also F 12 Kalmar, or simply F 12, is a former Swedish Air Force wing with the main base located on the south-east coast of Sweden. History The wing started out with three squadrons of B 17C in 1942. In 1947, F 12 was converted to a fighter wing by replacing the light bombers with the J 21A-2 which were upgraded to -3 before they were obsolete. Through 1952 to 1953, the three wings replaced the J 21's with J 29As which were only kept for five years until they were replaced by the J 32B Lansen in 1958. However, one of the squadrons were decommissioned after only two years. In 1962, the Air Force Meteorology School moved to F 12 Kalmar from F 2 Hägernäs. The two squadrons were upgraded to J 35F in 1968 which were kept until the decommissioning of the wing in 1980. The base with the meteorology school continued to operate under the F 17K name as a detachment to Blekinge Wing (F 17) until 1983 when the school moved to the Swedish A ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Focke-Wulf Fw 44
The Focke-Wulf Fw 44 ''Stieglitz'' ("Goldfinch") is a 1930s German two-seat biplane. An early design by Kurt Tank, it was produced by the Focke-Wulf company as a pilot training and sports flying aircraft. It was also eventually built under license in several other countries. Design and development The Fw 44 was designed as a biplane with conventional layout and straight, untapered wings. Its two open cockpits were arranged in tandem, and both cockpits were equipped with flight controls and instruments. The Fw 44 had fixed tailwheel landing gear. It employed ailerons on both upper and lower wings. It did not use flaps. It was flown with a Siemens-Halske Sh 14 radial engine. The first prototype flew in 1932. After many tests and modifications to increase the plane's durability and aerodynamics, the final Fw 44 proved to have excellent airworthiness. A second version of the Fw 44 was the Fw 44B, which had an Argus As 8 four-cylinder inverted inline air-cooled engine of 90 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
F 2 Hägernäs
Roslagen Air Corps ( sv, Roslagens flygkår), also F 2 Hägernäs, or simply F 2, is a former Swedish Air Force air corps with the main base located on the east coast of Sweden just north of the capital Stockholm. History From 1919 the area was used for flight training for navy pilots. The wing started out as the 2nd Flying Corps in 1926 with seaplanes for naval scouting and reconnaissance and bomb and torpedo attacks. In 1936 the unit was designated F 2 as an Air Force wing. A squadron of Heinkel T 2 (He 115) served between 1939 and 1944 and another squadron of Heinkel S 12 (He 114) between 1941 and 1945. The last operational flying squadron at F 2 consisted of Saab S 17BS reconnaissance floatplanes from 1942 to 1949 when the wing was renamed Roslagens Flygkår, ''Roslagen Flying Corps''. The wing then became home for various other operational units in the Air Force. The unit became home to the naval rescue unit until it moved to Svea Wing (F 8) in 1960. From 1948, the Rada ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Saab Tunnan
The Saab 29 ''Tunnan'', colloquially ''Flygande tunnan'' or just ''Tunnan'' ( en, "The flying barrel", "The barrel"),. is a Sweden, Swedish fighter aircraft, fighter that was designed and manufactured by Saab Group, Saab in the late 1940s. 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 post World War II, only being preceded in Western Europe as a whole by the Me 262 built during the war.Boyne 2002, p. 547."1940s." ''Saab'', Retrieved: 27 March 2016. Despite its rotund appearance, from which its name is derived, the J 29 was fast and agile and served effectively in both fighter and fighter-bomber roles into the 1970s. Development Sweden had fallen behind the rapid technical p ...[...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Wing (air Force Unit)
In military aviation, a wing is a unit of command. In most military aviation services, a wing is a relatively large formation of planes. In Commonwealth of Nations, Commonwealth countries a wing usually comprises three Squadron (aviation), squadrons, with several wings forming a group (air force unit), group (around 10 squadrons). Each squadron will contain around 20 planes. Commonwealth usage Origins On its establishment in 1912, the United Kingdom, British Royal Flying Corps (RFC) was intended to be an inter-service, combined force of the British Army and Royal Navy. Given the Interservice rivalry, rivalry that existed between the army and navy, new terminology was used, in order to avoid marking the corps out as having an army or navy ethos. While Cavalry wing, the term "wing" had been used in the cavalry, its more general use predominated. Accordingly, the word "wing", with its allusion of flight, was chosen as the term of subdivision and the corps was split into a " ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Sparmann S-1
__NOTOC__ The Sparmann S-1 was a 1930s Swedish military training monoplane, designed by Edmund Sparmann, built in small numbers for the Swedish Air Force. The S-1 was a single-seat low-wing braced-monoplane with a fixed trail-skid landing gear. It was powered by a single 130 hp (97 kW) de Havilland Gipsy Major engine. Operators ; :Swedish Air Force The Swedish Air Force ( sv, Svenska flygvapnet or just ) is the air force branch of the Swedish Armed Forces. History The Swedish Air Force was created on 1 July, 1926 when the aircraft units of the Army and Navy were merged. Because of the es ... Specifications See also References Further reading * * {{cite book , title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), publisher= Orbis Publishing 1930s Swedish military trainer aircraft ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
DFS Weihe
The DFS Weihe (English: ''Harrier'') is a German single-seat, high-wing, 18 metre wingspan, high-performance glider that was designed by Hans Jacobs in 1937-38. Design and development Jacobs designed the Weihe to be the pre-eminent performance glider of its era and indeed it captured many championships and set many records, until its performance was surpassed at the end of the 1950s. Even today it is considered one of the "classic sailplane designs". The Weihe is of wooden construction with fabric covering on the wing trailing edges and the control surfaces. The spar is built from Baltic Pine, with a birch leading edge D-box, fuselage and the fixed portions of the tail surfaces. The airfoil is a modified Gö 549-M.2 section. Early versions took off from a dolly and landed on a fixed skid, while later versions has a fixed wheel and skid undercarriage. Originally fitted with DFS-style airbrakes, some were later modified for Schempp-Hirth style brakes instead. The aircraft incor ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
DFS Kranich
The DFS Kranich is a type of German glider. It was developed by Hans Jacobs for the Deutsche Forschungsanstalt für Segelflug (DFS). History Series production of the Kranich (Crane) took place in the aircraft division of Karl Schweyer AG in Mannheim. The two-seater was, in its version 2, the most widely built two-seat glider in Germany from 1935 to 1939. Several hundred examples were built; exact numbers are not known. On 11 October 1940 Erich Klöckner in a Kranich achieved the record height in a glider of 11,460 m (37598 ft). Because it occurred in wartime, the altitude record was not recognized by the Allied occupying powers, and Klöckner only received official recognition by the Fédération Aéronautique Internationale (FAI) in the late 1990s.aerokurier magazine 1/1999: Erich Klöckners Vorstoß zur Tropopause, Motor Presse 1999 This record height was only exceeded ten years after the flight by the American Bill Ivans during a similar scientific program in the Sierra Ne ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Schneider Grunau Baby
The Schneider Grunau Baby was a single-seat sailplane first built in Germany in 1931, with some 6,000 examples constructed in some 20 countries. It was relatively easy to build from plans, it flew well, and the aircraft was strong enough to handle mild aerobatics and the occasional hard landing. When the Baby first appeared, it was accepted wisdom that the pilot should feel as much unimpeded airflow as possible, to better sense rising and falling currents of air and temperature changes etc. It was designed by Edmund Schneider with the assistance of Wolf Hirth and Hugo Kromer as a smaller version of Schneider's ESG 31 of the previous year, incorporating an elliptical wing design based on work done by Akaflieg Darmstadt. It was named after Grunau, the town where Schneider's factory was located, now Jeżów Sudecki in Poland. The first 14 inner ribs were of the Göttingen 535 shape with the outer ribs gradually changing up to the last 22nd rib, having a bi-convex and symmetric ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
DFS SG 38 Schulgleiter
The Schneider DFS 108-14 SG-38 ''Schulgleiter'' () is a German high-wing, cable-braced, single-seat primary glider that was designed by Schneider, Rehberg and Hofmann at Edmund Schneider's factory at Grunau in 1938, hence the designation. It was produced by several builders, including Deutsche Forschungsanstalt für Segelflug (DFS). Design and development The SG 38 was designed to be a training glider for basic flight training by the Nationalsozialistisches Fliegerkorps (NSFK). The usual launch method was by bungee cord from a sloped hill. Because training was conducted solely by solo flight the aircraft had to be very easy to fly and also easy to repair. The high-wing design uses a kingpost and cable bracing. The primary structure of the glider is of wood, with the wings, tail surfaces and inverted "V" kingpost all finished in doped aircraft fabric covering. The pilot sits on a simple seat in the open air, without a windshield. The basic configuration was similar to earli ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Saab 91 Safir
The Saab 91 Safir (Swedish for sapphire) is a three (91A, B, B-2) or four (91C, D) seater, single engine trainer aircraft. The Safir was built by Saab AB in Linköping, Sweden (203 aircraft) and by '' De Schelde'' in Dordrecht, Netherlands (120 aircraft). Design and development Development of the Safir began in 1944 as part of a plan to compensate for reductions in orders for military aircraft when the Second World War finally ended. Three major civil programmes were planned, the Type 90 Scandia airliner, the Type 91 Safir light aircraft and the Saab 92 motor car. The Safir was designed by Anders J. Andersson, who had previously worked for Bücker, where he had designed the all-wood Bücker Bü 181 "Bestmann". The Safir thus shared many conceptual design features with the Bestmann. It was primarily of metal construction, although it did have fabric-covered control surfaces. Development was slowed by the need to concentrate on more urgent military work, and by industrial actio ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
