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Hobby Master – Eurofighter FGR4 Typhoon , ‚ZK343‘ No. 1(F) Sqn, Royal Air Force , RAF Lossiemouth 2020

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                            Eurofighter Typhoon

Eurofighter Typhoon je dvoumotorový víceúčelový letoun s delta křídlem a kachními plochami, navržený a postavený konsorciem společností Alenia Aeronautica, BAE Systems a EADS, pracující jako holding Eurofighter GmbH (založeno v roce 1986). Projekt je řízen NATO Eurofighter and Tornado Management Agency, která je hlavním zákazníkem.

The Eurofighter Typhoon is a twin-engine, canard–delta wing, multirole fighter. The Typhoon was designed originally as an air superiority fighter 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 formed in 1986. NATO Eurofighter and Tornado Management Agency manages the project and is the prime customer.

Role Multirole fighter
National origin Multi-national
Manufacturer Eurofighter Jagdflugzeug GmbH
First flight 27 March 1994
Introduction 4 August 2003
Status In service
Primary users Royal Air Force
German Air Force
Italian Air Force
Spanish Air Force
See Operators below for others
Produced 1994–present
Number built 558
Unit cost
€90 million (system cost Tranche 3A)
£125 million (including development + production costs)
Developed from British Aerospace EAP
Variants Eurofighter Typhoon variants

General characteristics

  • Crew: 1 (operational aircraft) or 2 (training aircraft)
  • Length: 15.96 m (52.4 ft)
  • Wingspan: 10.95 m (35.9 ft)
  • Height: 5.28 m (17.3 ft)
  • Wing area: 51.2 m² (551 sq ft)
  • Empty weight: 11,000 kg (24,000 lb)
  • Loaded weight: 16,000 kg  (35,270 lb)
  • Max. takeoff weight: 23,500 kg (51,800 lb)
  • Fuel capacity: 5,000 kg (11,020 lb) internal
  • Powerplant: 2 × Eurojet EJ200 afterburning turbofan
    • Dry thrust: 60 kN (13,500 lbf) each
    • Thrust with afterburner: >90 kN (20,230 lbf) each

Performance

  • Maximum speed: **At altitude: Mach 2 class (2,495 km/h or 1,550 mph at 10,975m altitude)
    • At sea level: Mach 1.25 (1,530 km/h or 950 mph)
    • Supercruise: Mach 1.5
  • Range: 2,900 km (1,800 mi)
  • Combat radius:
    (with 3 × external 1,000 l tanks)

    • Ground attack, lo-lo-lo: 601 km (325 nmi)
    • Ground attack, hi-lo-hi: 1,389 km (750 nmi)
    • Air defence with 3-hr combat air patrol: 185 km (100 nmi)
    • Air defence with 10-min. loiter: 1,389 km (750 nmi)
  • Ferry range: >3,790 km (2,350 mi; with 3 × drop tanks)
  • Service ceiling: 19,812 m (65,000 ft)
  • Rate of climb: >318 m/s (62,600 ft/min)
  • Wing loading: 312 kg/m² (63.9 lb/ft²)
  • Thrust/weight: 1.15 (interceptor configuration)
  • g-load limits: +9 g to −3 g
  • Brakes-off to Take-off acceleration: <8 s
  • Brakes-off to supersonic acceleration: <30 s
  • Brakes-off to Mach 1.6 at 11,000 m (36,000 ft): <150 s

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