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The Schleicher K 8 is a single-seat glider designed by Rudolf Kaiser and built by the Alexander Schleicher company of Germany.
The Slingsby Type 42 Eagle was a two-seat glider designed in England from 1952.
The Neiva B Monitor, also designated B-2, is a Brazilian tandem two-seat glider aircraft designed and manufactured by Indústria Aeronáutica Neiva between 1945 and 1955 for primary training and general flying.
The Slingsby T.25 Gull 4 is a British glider designed and built by Slingsby that first flew in 1947.
The Slingsby T.30 Prefect is a 1948 British modernisation of the 1932 single-seat Grunau Baby glider. About 53 were built for civil and military training purposes.
The Slingsby Type 45 Swallow was designed as a club sailplane of reasonable performance and price. One of the most successful of Slingsby's gliders in sales terms, over 100 had been built when production was ended by a 1968 factory fire.
The Slingsby T.50 Skylark 4 was a British single seat competition glider built by Slingsby Sailplanes in the early 1960s. It sold in numbers and had success at national, though not world level competition.
The Civil Aviation Department RG-1 Rohini is an Indian two-seat training sailplane of the 1960s. A high-winged wooden monoplane, with side-by-side seating;at least 107 were built.
The Oberlerchner Mg 23 is a single-seat, all-wood, high-performance sailplane. It was built and first flown in Austria in 1955, and a total of 26 were built before production ended in 1965.
The Wassmer WA-30 Bijave is a French two-seat advanced training glider designed and built by Wassmer Aviation of Issoire.
The Bréguet Br 905 Fauvette is a single-seat, standard class, competition sailplane, designed and produced in France from the late 1950s. Some 50 were built but most remained grounded after a structural accident in 1969; a few remain airworthy.
The Cijan-Obad Orao is a competition single seat sailplane designed in Yugoslavia just after World War II, one of the most advanced of its type at the time. It flew in three World Gliding Championships, having greatest success at its first in 1950 when it reached third place.
The Rubik R-25 Mokány, in English: Plucky person and sometimes known as the R-25 Standard (class), is a Hungarian single seat Standard Class glider of all-metal construction, first flown in 1960. It was one of a series of similar aircraft designed by Ernő Rubik. Only one was built.
The Wassmer WA 20 Javelot and its very similar successors the WA 21 Javelot II and WA 22 Super Javelot are single seat gliders built in France in the 1950s and 1960s. Well over a hundred were sold as club aircraft and over fifty remain on the French civil register in 2010.
The Horikawa H-23B-2 is a two-seat training glider designed and built in Japan in the 1950s. It was produced in small numbers.
The Lie-Fang 1, some sources Jeifang 1, was one of the first gliders designed and built in China, though with Polish design input. It is an all-wood, two seat, intermediate training aircraft which first flew in 1958.
The Antonov A-11 is a single-seat, high performance, all-metal sailplane built in the Soviet Union in the late 1950s. 150 were produced.
The Győr-2 was a high performance sailplane designed and built at the Aircraft Designer and Builder Group, Aeroclub of the Rolling-stock Factory, Győr in Hungary in the early 1950s.
The UTG-1 Loudon was an intermediate glider designed and built at the University of Toronto in Canada during the late 1940s.
The Bruni 3V-1 Eolo was a single seat Italian competition glider, first flown in 1955. It took part World Gliding Championships of 1956 but retired early after sustaining damage.
References
- 1 2 3 Bridgman, Leonard (1956). Jane's All the World's Aircraft 1956-57. London: Jane's All the World's Aircraft Publishing Co. Ltd. pp. 42–3.
- ↑ Shenstone, B.S.; K.G. Wilkinson; Peter Brooks (1958). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde (in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 9–13.