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The Eurofighter Typhoon is a European multinational twin-engine, supersonic, canard delta wing, multirole fighter. [3] [4] The Typhoon was designed originally as an air-superiority fighter [5] and is manufactured by a consortium of Airbus, BAE Systems and Leonardo that conducts the majority of the project through a joint holding company, Eurofighter Jagdflugzeug GmbH.
The Typhoon T1 is a Tranche 1, batch 1 two-seat trainer. The first Typhoon T1 is one of the Instrumented Production Aircraft (IPA1) and remains part of the BAE fleet. The aircraft's maiden flight was on 15 April 2002. The official in service date for the first RAF Typhoon T1, serial ZJ803, was 30 June 2003. [25] [unreliable source?
Eurofighter offered its latest version of the Typhoon, equipped with Captor-E AESA radar, for Indonesia's F-5 replacement programme. [166] In a letter to the Austrian Minister of Defence , Indonesia expressed willingness to buy its entire fleet of 15 Typhoons that have been operating in the Austrian Air Force since 2008.
Eurofighter EF2000 with both EJ200s in full reheat DECU/DECMU of a Eurojet EJ200D engine. The Eurojet EJ200 is a military low-bypass turbofan used as the powerplant of the Eurofighter Typhoon. The engine is largely based on the Rolls-Royce XG-40 technology demonstrator, which was developed in the 1980s.
ANKARA (Reuters) -Turkey began talks with European states on buying 40 Eurofighter Typhoon jets after recognising that its request for F-16 jets from the United States might not work out, a ...
The EJ200 engine built by EuroJet Turbo GmbH mounted in the Eurofighter Typhoon. It is capable of supercruising at Mach 1.5 with an air superiority missile load. [16] Typhoon pilots have stated that Mach 1.3 is attainable in combat configuration with external stores. [21]
The origins of the EAP can be found within the Agile Combat Aircraft (ACA) programme performed by British Aerospace (BAe) during the late 1970s and early 1980s. [2] [3] It is known that ACA had involved the combining of several years of private venture research conducted by BAe, costed at around £25 million, together with similar contemporary studies that had been performed by West German ...
The top speed was calculated as 509 mph (819 km/h) at 20,000 ft, with a rate of climb of 6,400 ft/min (1,951 m/min). Service ceiling was projected to be more than 42,000 ft (13,000 m). [ 51 ] Work on both was ultimately dropped when Camm decided to focus design efforts upon the more promising jet engine designs he was working on instead.