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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 thrust-to-weight ratio is usually calculated from initial gross weight at sea level on earth [6] and is sometimes called thrust-to-Earth-weight ratio. [7] The thrust-to-Earth-weight ratio of a rocket or rocket-propelled vehicle is an indicator of its acceleration expressed in multiples of earth's gravitational acceleration, g 0. [5] The ...
EJ200 displayed at ILA Berlin Air Show 2018. The Eurojet consortium was formed in 1986 to co-ordinate and manage the project largely based on XG-40 technology. In common with the XG-40, the EJ200 has a three-stage fan with a high pressure ratio, five-stage low-aspect-ratio high-pressure (HP) compressor, a combustor using advanced cooling and thermal protection, and single-stage HP and LP ...
Two pilots demonstrated the differences between the fighter jets, referencing dogfight footage and using quickly made paper airplanes. NATO fighter pilots break down their Eurofighter vs F-35 ...
The M-346, in the multirole Fighter Attack variant (M-346FA), is equipped with a multi-mode fire-control radar (Grifo M-346 by Leonardo Electronics) [25] and a total of seven hardpoints, it is capable of carrying external loads up to 3,000 kg while maintaining a high thrust-to-weight ratio; stores management data can be presented upon any of ...
The countries and companies behind Europe's Eurofighter Typhoon fighter jet have agreed to spend 53.7 million euros ($60.2 million) to study the long-term evolution of the advanced fighter jet and ...
The aircraft first flew on 6 April 1994 as ZH588. The flight control assessment included development of the Eurofighter's "carefree handling". On 23 December 1997 DA2 became the first Eurofighter to achieve Mach 2 and in January 1998 undertook refuelling trials with a RAF VC10. Like DA1, DA2 was upgraded in 1998 with new engines, ejector seat ...
Jet or rocket engine Mass Thrust Thrust-to-weight ratio (kg) (lb) (kN) (lbf) RD-0410 nuclear rocket engine [1] [2] 2,000 4,400 35.2 7,900 1.8 J58 jet engine (SR-71 Blackbird) [3] [4] 2,722 6,001 150 34,000 5.2 Rolls-Royce/Snecma Olympus 593 turbojet with reheat [5] 3,175 7,000 169.2 38,000 5.4 Pratt & Whitney F119 [6] 1,800 3,900 91 20,500 7.95