Author: Karol
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Airport in Mirosławiec. 2013.
On the basis of DWL Order No. 06 of February 23, 1982, the 3rd Brandenburg Reconnaissance Aviation Division was renamed the 3rd Fighter-Bomber Aviation Division. At the same time, the Division took over the 3rd Regiment of Fighter-Bomber Aviation from Bydgoszcz, using Su-7 planes. For the 8th Regiment in Mirosławiec, it was a time of…
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AI-24 turboprop engine
During the 50 years, the CCCP developed several turboprop engines. One of them was the Ivchenko AI-20 engine. This engine was used to power such aircraft as An-10, An-12 and Ił-18. The engine was developed at the end of the 50-year period in Zaporizhia. The team was headed by Alexander Ivchenko. Previously, the team was…
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Atar 9 turbojet engine
The French decided to radically rebuild the engine. The Atar 08 program was launched. The dimensions of the new engine have slightly improved. The compressor has grown from 7 stages to 9 stages. Compression increased to 5.5: 1. The turbine has been completely rebuilt, increasing its diameter. New alloys were introduced, including magnesium alloys. The…
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R-29 turbojet engine
The R-25 engine is a continuation of the R-11, R-13 engines. The R-25 engine was used in the MiG-21 bis aircraft. The R-25 engine has two levels of afterburning. The R-25-300 engine has 1 x 4,020 kG without afterburning thrust, 6,960 kG with the first afterburning, and 9,708 kG with the second afterburning. The engine…
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R-13 turbojet engine
The R-13 turbojet engine is a direct development of the R-11 engine, which was commonly used in MiG-21 aircraft. The engine was modernized under the supervision of S. Gawryłów. The aim of the modernization was to reduce fuel consumption, increase thrust and, above all, improve overall parameters.
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AI-25 turbojet engine
The history of Ivchenko’s aircraft engines began in 1945, at the Ukrainian CCCP in Zaporizhia. At that time, the OKB-478 design office and experimental plant were organized. The task of the OKB-478 office was to develop aircraft engines for airplanes and helicopters as well as other machines and devices for industry. The office was headed…
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R-11 turbojet engine
Information on Bristol Olimpus and General Electric J57 engines penetrated the CCCP. In 1952-1954, the Moscow Aviation Institute made aerodynamic calculations for a turbojet engine with a system of two shafts (propellers, spools). The calculations were carried out to achieve the speed of Ma 2 by the future aircraft. The main difficulty was to create…
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J79-GE turbojet engine
Movable aerodynamic blades of the compressor stator was one of the ways to improve the operation of the turbojet engine. General Electric has been considering for almost a year – Which concept to choose? In 1952, it was decided to use movable steering wheels. With this arrangement, it was easier to develop lubrication and sealing…
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AL-7 / AL-21 turbojet engine
An important engine in the CCCP was the AL-7 F-1 engine, which in Archip M. Lulka’s team was called TRD-31. The engine was created at the beginning of the 50s, through the development of the AL-5 engine, especially its enlargement. The AL-7 engine was first launched in September 1952. The AL-7 engine was used to…
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RD-9 turbojet engine
Aleksander Mikulin, in addition to the large AM-3 engine, also developed the AM-5 engine with a lower power. This task resulted from the collapse of the TR-3 engine program, which had high hopes. The fall of the TR-3 engine program also plunged airframe programs, including the supersonic Su-17 (the first program with such a designation).…
