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  2. Eurofighter Typhoon - Wikipedia

    en.wikipedia.org/wiki/Eurofighter_Typhoon

    The Eurofighter Typhoon is fitted with two Eurojet EJ200 engines, each capable of providing up to 60 kN (13,500 lbf) of dry thrust and >90 kN (20,230 lbf) with afterburners. Using the "war" setting, dry thrust increases by 15% to 69 kN per engine and afterburners by 5% to 95 kN per engine and for a few seconds, up to 102 kN thrust without ...

  3. Thrust-to-weight ratio - Wikipedia

    en.wikipedia.org/wiki/Thrust-to-weight_ratio

    Thrust-to-weight ratio is a dimensionless ratio of thrust to weight of a rocket, jet engine, ... Eurofighter Typhoon: 1.15 [15] Interceptor configuration Sukhoi Su-35:

  4. Eurojet EJ200 - Wikipedia

    en.wikipedia.org/wiki/Eurojet_EJ200

    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 ...

  5. Jet fighter generations - Wikipedia

    en.wikipedia.org/wiki/Jet_fighter_generations

    F/A-18, Su-30, J-10, Eurofighter Typhoon ... thrust-to-weight ratios greater than one (enabling the plane to climb vertically), hypermanoeuvrability, advanced digital ...

  6. NATO fighter pilots break down their Eurofighter vs F-35 ...

    www.aol.com/nato-fighter-pilots-break-down...

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  7. EuroJet Turbo GmbH - Wikipedia

    en.wikipedia.org/wiki/EuroJet_Turbo_GmbH

    The EJ200 engine combined the leading technologies from each of the four European companies, using advanced digital control and health monitoring; wide chord aerofoils and single crystal turbine blades; and a convergent / divergent exhaust nozzle to give excellent thrust-to-weight ratio, multimission capability, supercruise performance, low ...

  8. Eurofighter Typhoon variants - Wikipedia

    en.wikipedia.org/wiki/Eurofighter_Typhoon_variants

    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 and avionics and rejoined the test programme in August.

  9. Panavia Tornado - Wikipedia

    en.wikipedia.org/wiki/Panavia_Tornado

    Thrust/weight: 0.77; Armament. Guns: 1 × 27 mm (1.06 in) Mauser BK-27 revolver cannon internally mounted under starboard side of fuselage with 180 rounds [d] Hardpoints: 3 × under-fuselage and 4 × under-wing pylon stations [e] with a capacity of 9,000 kg (19,800 lb), with provisions to carry combinations of: Missiles: