Author: Karol
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Sukhoi Su-22 M 4 K nb 3818 accident on 1995-04-04.
The outbreak of the Second Cold War at the beginning of the 1980s forced the rearmament of the Warsaw Pact countries. In Poland, MiG-23 MF planes were introduced to the service of fighter aviation in a limited number and, for financial reasons, to two MiG-21 bis regiments. However, the real retooling took place in the…
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Aero-engines – Turbojets in Poland – Part 26
In the PZL WSK Rzeszów in the 1950s turbojet engines under Lis-1, Lis-2 and Lis-5 licenses were built. These engines were used to propel Lim-1, Lim-2, Lim-5 and Lim-6 bis aircraft. In Poland, it was hoped that the MiG-21 fighter aircraft, as Lim-7, would be produced in PZL Mielec, and the Tumański R-11 engine in…
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Grudziądz Airport. 2017
The airport in Grudziądz was established in 1911, using a flat area to the south-east of the city center, so far used as a cavalry training ground. The airport hindered the expansion of the city. In 1980, construction of a new housing estate began near the airport and as a result, the airport was closed.
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Leonardo M-346 Bielik. 2016.
The M-346 Master – Bielik is an advanced training training aircraft. It was adopted by the Polish Army. On November 14, 2016, the first two Leonardo M-346 Master planes – Bielik Nb 7702 and 7703 – landed in Dęblin.
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Aircraft Engines – Turbo-Fan – Part 22
The General Electric CF6 commercial engine became a development of the General Electric TF39 engine. Its first launch took place in 1971. It was used as a drive for B747, B767, DC-10, A300, A310, A330 and others. The entire family of CF6 engines was created, from which subsequent generations of turbo-fan engines developed.
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Aircraft Engines – Turbojets – Part 20
The Pratt & Whitney F-100 engine used in the F-15 and F-16 aircraft was a great success in military aviation. In 1962, the research and development work of the USAF and NAVA were merged. The goal was to cut costs. As a result, in 1967, USAF and NAVY issued joint requirements for a new engine…
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Aircraft Engines – Turbojets in France – Part 21
Atar 9 engine data: The single-flow, single-shaft motor received a 9-stage axial compressor. Compressor 5.2: 1 compression. Combustion chamber. 2-stage turbine. Afterburner. Length 5.90 m, diameter 1.00 m, weight 1,456 kg. 42.00 kN draft without afterburning and 58.90 kN with afterburning. Air flow through the engine 68 kg / s. fuel consumption 103 kg /…
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Aircraft Engines – Turbojets – Part 19
The JT3D / TF33 engine is a development of the JT3C / J57 engine by making it in the two-flow technology. The engine was developed by the airlines for the B 707 aircraft. Work on it started in 1957. The first operational use of the propulsion took place on June 22, 1960, when the first…
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Aircraft Engines – Turbojets in CCCP – Part 18
Aleksander Mikulin developed the AM-5 engine. The AM-5 engine was created in 1951 and was a scaled down AM-3 engine. The power, as well as dimensions and weight were reduced, which allowed to place this engine in a fighter class airframe. Alexander Mikulin’s team worked under time pressure. The lag of CCCP in turbojet engines…
