badge icon

This article was automatically translated from the original Turkish version.

Article

Eurofighter Typhoon

resim_2025-04-16_202802122.png
First Flight / Entry into Service
27 March 19944 August 2003
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Aircraft Type
Multirole Fighter
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Maximum Altitude
19812 metres (65000 ft)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDeployable Radar Jammer)
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Maximum Thrust
Each engine with afterburner: 90 kN (20000 lbf)
Aircraft Type
Multirole Fighter
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maximum Altitude
19812 metres (65000 ft)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maximum Thrust
90 kN (20000 lbf) per engine with afterburner
First Flight / Service Entry
27 March 1994 / 4 August 2003
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDeployable Radar Decoys)
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Maximum Altitude
19812 metres (65000 ft)
Maximum Altitude
19812 metres (65000 ft)
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Maximum Thrust
90 kN (20000 lbf) per engine with afterburner
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in certain configurations
First Flight / Service Entry
27 March 1994 / 4 August 2003
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Aircraft Type
Multirole Fighter
Aircraft Type
Multirole Fighter Aircraft (Multirole Fighter)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Aircraft Type
Multirole Fighter Aircraft (Multirole Fighter)
First Flight / Service Entry
27 March 1994 / 4 August 2003
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Maximum Altitude
19812 metres (65000 ft)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Aircraft Type
Multirole Fighter Aircraft (Multirole Fighter)
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Maximum Altitude
19812 metres (65000 ft)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Aircraft Type
Multirole Fighter
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
First Flight / Service Entry
27 March 1994 / 4 August 2003
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability without afterburner at Mach 1.5 in specific configurations
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maximum Altitude
19812 metres (65000 ft)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability without afterburner at Mach 1.5 in specific configurations
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDeployable Radar Jammer)
First Flight / Entry into Service
27 March 1994 / 4 August 2003
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Aircraft Type
Multirole Fighter Aircraft (Multirole Fighter)
Maximum Altitude
19812 metres (65000 ft)
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDeployable Radar Decoys)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
First Flight / Entry into Service
27 March 1994 / 4 August 2003
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in certain configurations
Aircraft Type
Multirole Fighter Aircraft (Multirole Fighter)
First Flight / Entry into Service
27 March 1994 / 4 August 2003
Maximum Altitude
19812 metres (65000 ft)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Aircraft Type
Multirole Fighter Aircraft (Multirole Fighter)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Producer Consortium
Eurofighter Jagdflugzeug GmbH
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDeployable Radar Jammer)
Main Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Main Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Producer Consortium
Eurofighter Jagdflugzeug GmbH
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDeployable Radar Jammer)
Maximum Altitude
19812 metres (65000 ft)
First Flight / Service Entry
27 March 1994 / 4 August 2003
Aircraft Type
Multirole Fighter Aircraft
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maximum Altitude
19812 metres (65000 ft)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Producer Consortium
Eurofighter Jagdflugzeug GmbH
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Main Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Electronic Warfare (EW)
Praetorian DASS (Electronic CountermeasuresECMDeployable Radar Jamming)
First Flight / Service Entry
27 March 1994 / 4 August 2003
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
First Flight / Service Entry
27 March 1994 / 4 August 2003
Electronic Warfare (EW)
Praetorian DASS (Electronic CountermeasuresECMDeployable Radar Jamming)
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Producer Consortium
Eurofighter Jagdflugzeug GmbH
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Maximum Altitude
19812 metres (65000 ft)
Main Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Aircraft Type
Multirole Fighter Aircraft (Multirole Fighter)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maximum Altitude
19812 metres (65000 ft)
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMTowed Radar Decoy)
First Flight / Service Entry
27 March 1994 / 4 August 2003
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system.
Aircraft Type
Multirole Fighter Aircraft (Multirole Fighter)
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Main Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Maximum Altitude
19812 metres (65000 ft)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMTowed Radar Decoy)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system.
Engine
2 x Eurojet EJ200 turbofan (produced by the Eurojet Consortium)
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
First Flight / Service Entry
March 271994 / August 42003
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Aircraft Type
Multirole Fighter Aircraft
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability without afterburner at Mach 1.5 speed in specific configurations
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDrag Radar Decoy)
Maneuverability
Delta wing with aerodynamically unstable design and quadruple-redundant fly-by-wire (FBW) control system.
Maximum Altitude
19812 metres (65000 feet)
Engine
2 x Eurojet EJ200 Turbofan (produced by the Eurojet Consortium)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
First Flight / Service Entry
March 271994 / August 42003
Maximum Thrust
Each motor art burner produces 90 kN (20000 lbf)
Aircraft Type
Multirole Fighter Aircraft
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Engine
2 x Eurojet EJ200 turbofan (produced by the Eurojet Consortium)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Cruise capability at Mach 1.5 without afterburner (Supercruise) in certain configurations
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
First Flight / Entry into Service
27 March 1994 / 4 August 2003
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMTowed Radar Decoy)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Maximum Altitude
19812 metres (65000 ft)
Aircraft Type
Multirole Fighter Aircraft
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Aircraft Type
Multirole Fighter Aircraft
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMTowed Radar Decoy)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Engine
2 x Eurojet EJ200 Turbofan (produced by EUROJET Consortium)
First Flight / Entry into Service
27 March 1994 / 4 August 2003
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in certain configurations
Maximum Altitude
19812 metres (65000 ft)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Electronic Warfare (EW)
Praetorian DASS (Electronic CountermeasuresECMTowed Radar Decoy)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Engine
2 x Eurojet EJ200 turbofan (produced by the Eurojet Consortium)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Primary Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Aircraft Type
Multirole Fighter Aircraft
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Maximum Altitude
19812 metres (65000 ft)
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in certain configurations
First Flight / Service Entry
27 March 1994 / 4 August 2003
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in certain configurations
Maximum Altitude
19812 metres (65000 ft)
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Aircraft Type
Multirole Fighter Aircraft
First Flight / Service Entry
27 March 1994 / 4 August 2003
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Electronic Warfare (EW)
Praetorian DASS (Electronic CountermeasuresECMTowed Radar Decoy)
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Main Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Maximum Altitude
19812 metres (65000 ft)
First Flight / Service Entry
27 March 1994 / 4 August 2003
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDeployable Radar Jammer)
Engine
2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium)
Maneuverability
Canard-delta wingaerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system
Speed / Supercruise
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in specific configurations
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
Manufacturer Consortium
Eurofighter Jagdflugzeug GmbH
Main Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Aircraft Type
Multirole Fighter Aircraft
Basic Dimensions
Length: 15.96 m / Wingspan: 10.95 m / Height: 5.28 m
Electronic Warfare (EW)
Praetorian DASS (Electronic Support MeasuresECMDeployable Radar Jammer)
Aircraft Type
Multirole Fighter Aircraft
Speed / Supersonic
Maximum: Mach 2.0 (2495 km/h) / Supercruise capability at Mach 1.5 without afterburner in certain configurations
First Flight / Entry into Service
27 March 1994 / 4 August 2003
Main Industrial Partners
Airbus (GermanySpain)BAE Systems (United Kingdom)Leonardo (Italy)
Maximum Altitude
19812 metres (65000 ft)
Producer Consortium
Eurofighter Jagdflugzeug GmbH
Maximum Thrust
Each engine with afterburner produces 90 kN (20000 lbf)
Project Management
NATO Eurofighter and Tornado Management Agency (NETMA)
First Flight / Entry into Service
27 March 1994 / 4 August 2003

Eurofighter Typhoon is a twin-engine, supersonic, canard-delta wing multirole fighter aircraft developed by Eurofighter GmbH, a consortium of Europe’s leading aerospace companies: Airbus (Germany and Spain), BAE Systems (United Kingdom), and Leonardo (Italy). The program has been shaped since its inception by complex layers of challenges including Cold War dynamics, national budget constraints, and intricate international workshare negotiations. Although initially designed as an air superiority fighter, extensive modernization programs implemented during its operational service life (known as Tranches) have transformed it into a fully integrated ground attack and electronic warfare platform. This evolution has strengthened the aircraft’s strategic role within national air forces and enhanced its competitiveness in the global market.


Foundations of the Development Program

The foundations of the Eurofighter program were laid in 1979 with the European Combat Aircraft (ECF) studies initiated by France, the United Kingdom, and West Germany. These efforts evolved in 1983 into the Future European Fighter Aircraft (FEFA) program, with the participation of France, the United Kingdom, Germany, Italy, and Spain. However, deep disagreements emerged in later stages regarding the aircraft’s design requirements. France advocated for a lighter, single-engine platform primarily suited for carrier operations (ultimately resulting in the Dassault Rafale), while the other partners insisted on a heavier, twin-engine air superiority fighter. This disagreement led to France’s withdrawal from the consortium in 1985 to pursue its national project, while the remaining four nations united under the European Fighter Aircraft (EFA) program. The technology demonstrator for the program, the British Aerospace EAP (Experimental Aircraft Programme), made its first flight in 1986 and established the foundational design of the canard-delta configuration. The first EFA prototype (DA1) flew in 1994, and the aircraft was officially named Typhoon in 1998.


Germany’s Withdrawal Attempt

During the development phase, Germany faced significant pressure in the early 1990s due to the heavy financial burden of reunification. Chancellor Helmut Kohl publicly threatened to cancel the Eurofighter project, while Defense Minister Volker Rühe proposed in early 1991 that Germany withdraw from the program and transition to a cheaper, lighter aircraft based on Eurofighter technology.


However, this withdrawal attempt failed. The substantial financial investment already made in the development phase, the tens of thousands of jobs dependent on the program, and most critically, binding and penalizing contractual agreements signed among the partner governments, prevented Germany from unilaterally exiting. This system of contractual penalties, established by Rühe’s predecessors, proved decisive in ensuring the program’s continuation despite Kohl’s political will.


Workshare Disputes and Production Contract

In 1995, new tensions arose over workshare balances due to changes in order quantities. When Eurofighter GmbH was established, workshare had been allocated according to initial order commitments: United Kingdom 33%, Germany 33%, Italy 21%, and Spain 13%.

However, as all nations reduced their initial orders (UK from 250 to 232, Germany from 250 to 140, Italy from 165 to 121, Spain from 100 to 87), the workshare needed to be realigned according to the new order ratios. Theoretically, the revised shares should have been: UK 39%, Germany 24%, Italy 22%, and Spain 15%. Germany resisted such a significant reduction in its share.


After prolonged negotiations, an agreement was reached in January 1996 between British and German partners: Germany committed to purchasing an additional 40 aircraft to preserve a workshare closer to the original agreement. As a result, the final workshare percentages were adjusted as follows: United Kingdom 37.42%, Germany 29.03%, Italy 19.52%, and Spain 14.03%. Following this agreement, on 22 December 1997, the defense ministers of the four partner nations signed the final contract to initiate series production of the aircraft.

Cooperation Structure and Supply Mechanism

The Eurofighter Typhoon program is structured around two main management bodies and four primary industrial partners.

Management and Customer Interface (NETMA)

  • NATO Eurofighter and Tornado Management Agency (NETMA): A NATO agency representing the four main customer nations, responsible for defining customer requirements and signing main contracts with industrial partners. NETMA’s responsibilities also include managing long-term evolution (Long Term Evolution - LTE) studies and engine supply contracts (with EUROJET).

Industrial Consortium (Eurofighter GmbH)

  • Eurofighter Jagdflugzeug GmbH: The company responsible for industrial management and production coordination of the program.
  • Primary Partners and Production Leadership:
    • Airbus Defence and Space (Germany/Spain): Responsible for the assembly of aircraft for the German Air Force (Luftwaffe) and the Spanish Air and Space Force (Ejército del Aire y del Espacio), as well as the production of associated airframe sections. Germany’s Manching facility is one of these assembly lines.
    • BAE Systems (United Kingdom): Conducts final assembly of Royal Air Force (RAF) aircraft at its Warton facility. It also plays a leading role alongside the UK government in potential export projects such as the Memorandum of Understanding (MoU) with Türkiye.
    • Leonardo S.p.A. (Italy): Conducts assembly of aircraft for the Italian Air Force (Aeronautica Militare) and is a consortium leader in avionics, radar, and electronic warfare systems.


Engine Cooperation (EUROJET) and Shares

The aircraft’s heart, the EJ200 turbofan engines, are developed and produced by a separate consortium: EUROJET Turbo GmbH.

  • Partners: Rolls-Royce (UK), MTU Aero Engines (Germany), Avio Aero (Italy), and ITP Aero (Spain).
  • Workshare and Specialization Areas:
    • MTU Aero Engines: Responsible for the development and production of the low- and high-pressure compressors and the Digital Engine Control and Monitoring Unit (DECMU). It also performs final engine assembly for German and Austrian aircraft.
    • Avio Aero: Responsible for the production of the engine’s critical component, the Low-Pressure Turbine, and the Accessory Drive Gearbox (AMAD), as well as maintenance, repair, and overhaul (MRO) services for the Italian Air Force fleet.


This cooperation model ensures that all partners benefit economically, even in large acquisitions such as Germany’s Tranche 5 order, by requiring hundreds of new engine supply contracts to be signed between EUROJET and NETMA.

Technical Specifications

The Eurofighter Typhoon is a fourth-generation and beyond (4.5 generation) fighter aircraft integrating innovative solutions in avionics, aerodynamics, and materials technology.

Aerodynamics and Airframe Structure

The Typhoon employs a canard (foreplane) and delta wing configuration to achieve superior maneuverability at high angles of attack and supersonic speeds. This aerodynamic design deliberately renders the aircraft statically unstable, necessitating a highly advanced Quadruple-Redundant Fly-by-Wire (FBW) system. The FBW continuously manages flight control, enabling the pilot to maintain precise handling even during high-G maneuvers.

  • Dimensions and Weight: Length is 15.96 meters, wingspan is 10.95 meters, and maximum takeoff weight is approximately 23,500 kg.
  • Material Usage: A large portion of the airframe is constructed from lightweight, radar-absorbent materials such as carbon fiber composites and glass-reinforced plastics to reduce radar cross-section (RCS). Only 15% of the airframe surface consists of metallic components.

Performance

  • Speed: The aircraft can reach a maximum speed of Mach 2.0 (approximately 2,495 km/h) at high altitude and Mach 1.25 at sea level.
  • Supercruise: The EJ200 engines enable sustained supersonic cruise (Supercruise) at around Mach 1.5 without afterburner, under specific configurations (typically with light weapon loads). This capability is critical for extending operational range and reducing response time.
  • Range and Altitude: Internal fuel provides a range of approximately 2,900 km, extendable through aerial refueling. Service ceiling is 19,812 meters (65,000 ft).


Avionics and Sensing Systems

The Typhoon is equipped with an advanced avionics suite designed to provide pilots with comprehensive situational awareness and effectively neutralize enemy threats. These systems have been integrated with significant contributions from Leonardo.

Radar Systems (Euroradar CAPTOR)

  • CAPTOR-M (M-Scan): A mechanically scanned (MSA) Pulse Doppler radar system used in initial production batches (Tranche 1–3).
  • ECRS (European Common Radar System) Family: Represents the transition to Active Electronically Scanned Array (AESA) technology.
    • ECRS Mk0/Radar 1: The first AESA radar system delivered to export customers such as Kuwait and Qatar. It features a mechanical re-positioner, providing a wider field of regard (approximately 200 degrees) than conventional AESA radars.
    • ECRS Mk2 (Radar 2): Developed under UK leadership, this multirole AESA variant integrates powerful Electronic Warfare (EW) and Electronic Attack (EA) capabilities alongside traditional radar functions. This system aims to significantly enhance the aircraft’s ability to control the electromagnetic spectrum in future missions.

PIRATE IRST and Passive Sensing

The PIRATE IRST (Passive Infrared Search and Track System) is located on the left side of the nose. Its passive operation, which emits no electromagnetic signals, reduces the aircraft’s risk of detection while enabling long-range target detection and tracking. PIRATE can be used for air-to-air (multi-target tracking) and air-to-ground (target identification/lock-on) roles and provides infrared imaging for visual identification.

Praetorian DASS and Electronic Warfare

The Praetorian DASS (Defensive Aids Sub-System) was developed by the EuroDASS consortium.

  • Components: DASS is housed in wingtip pods and includes Electronic Support Measures (ESM), Missile Approach Warners (MAW), jamming (ECM) systems, and towed radar decoys.
  • Function: The system detects and analyzes air-to-air and surface-to-air threats even in high-density electromagnetic environments and automatically or manually applies the most appropriate countermeasure. The ECM system uses DRFM (Digital Radio Frequency Memory) technology to copy and distort enemy radar signals, significantly enhancing the aircraft’s survivability.

Cockpit and Human-Machine Interface (HMI)

The cockpit is designed to maximize pilot situational awareness and control capability and includes the following features:

  • Display: Three color Multi-Function Head-Down Displays (MHDD) and a wide-angle Head-Up Display (HUD).
  • Controls: HOTAS (Hands-On Throttle-And-Stick) system and potential Direct Voice Input (DVI) voice command systems.
  • Striker II HMD: BAE Systems’ Helmet-Mounted Display (HMD) projects targeting symbology aligned with the pilot’s line of sight, enabling “off-bore sight” targeting. Integrated digital night vision and color symbology reduce pilot workload and facilitate friend-or-foe identification, particularly in intense combat environments.



Weapon Systems and Operational Applications

The Eurofighter Typhoon has the flexibility to carry up to 7,500 kg of ordnance across 13 external stations (five under the fuselage and eight under the wings) and serves as a fully integrated "swing-role" platform through the integration of modern munitions.

Air-to-Air and Air-to-Ground Capabilities

  • Air Defence: For long-range air combat it employs the MBDA Meteor (ramjet-powered BVRAAM) and AIM-120 AMRAAM missiles. For close-range air combat it is supported by the AIM-132 ASRAAM and IRIS-T missiles, enabling high maneuverability.
  • Air-to-Ground Strike: Strategic strike and deep interdiction missions are enabled by the integration of the Storm Shadow (cruise missile) and Taurus missiles. Anti-armour missions against tanks and armored targets are conducted using Brimstone missiles. Precision strikes are carried out with Paveway IV and GPS/laser-guided GBU series bombs.
  • Internal Weapon: 27 mm Mauser BK-27 rotary cannon.

Modernization Tranches

The aircraft’s service life and capabilities are managed through phased production and modernization tranches:

  • Tranche 1: The initial production block focused primarily on the Air Defence role.
  • Tranche 2: Integration of advanced avionics and air-to-ground capabilities began.
  • Tranche 3A/3B: Includes necessary hardware modifications and increased fuel capacity for future AESA radar and avionics upgrades.
  • Tranche 4 / Tranche 5: The most recent acquisitions, such as Germany’s Quadriga order, fall under this tranche. It focuses on the ECRS AESA radar, electronic warfare capability (Typhoon EK), and updated weapons integration.


The Eurofighter Typhoon is actively operated by the air forces of the United Kingdom, Germany, Italy, and Spain, as well as Austria, Saudi Arabia, Oman, Kuwait, and Qatar.


National Air Forces and Inventory Details

The Typhoon is currently operated by nine different air forces: the United Kingdom, Germany, Italy, Spain, Austria, Saudi Arabia, Oman, Kuwait, and Qatar.


Combat Experience and Role

Since entering operational service in 2003, the aircraft has participated in various international operations and demonstrated its multirole capabilities:

  • Operation Ellamy (2011, Libya): Marked the Typhoon’s first combat experience and demonstrated its ability to conduct air-to-ground strike missions even in Tranche 1 aircraft, alongside its air defence role.
  • Operation Shader (from 2015, Iraq and Syria): Deployed in coalition operations against ISIS, proving its effectiveness in close air support (CAS) and reconnaissance missions.
  • NATO Air Policing (QRA): Continuously conducted by the RAF, Luftwaffe, and Italian Air Force, the Quick Reaction Alert (QRA) missions, along with NATO’s air policing operations in the Baltic, Iceland, and Black Sea regions, contribute directly to the alliance’s collective defence efforts.

Strategic and Geopolitical Contribution

The Typhoon enables its operator nations to secure their own airspace while serving as a flexible and reliable platform in international interventions and NATO missions. The aircraft’s continuous modernization ensures that operator nations remain technologically current and maintain interoperability with other allied platforms such as the F-35.


Türkiye’s Eurofighter Typhoon Procurement and Cooperation Context

Türkiye’s interest in procuring the Eurofighter Typhoon is part of its broader effort to modernize its air power, particularly in response to uncertainties arising from the F-35 program.

Procurement Process and Agreement

Türkiye has initiated formal discussions with the United Kingdom regarding the potential procurement of up to 40 Typhoon combat aircraft. The first significant step in this process was the signing of a Memo of Understanding (MoU) between the defence ministries of the United Kingdom and Türkiye in 2025. This represents an official preliminary step in the procurement process.

Geopolitical Dimension of Cooperation and Consortium Approval

The Typhoon is a platform requiring full export approval from all four consortium countries (United Kingdom, Germany, Italy, Spain). Türkiye’s procurement process clearly highlights the industrial and geopolitical complexity of the program:

  • Germany’s Role: Negotiations have faced delays due to Germany’s longstanding reluctance to approve export licenses, primarily over concerns regarding Türkiye’s foreign policy. Germany’s approval is essential for any final contract to be signed.
  • Importance for British Industry: Türkiye’s potential order is critical to maintaining the active status of BAE Systems’ Warton assembly line in the United Kingdom prior to its transition to the GCAP program, and to preserving thousands of skilled jobs. Consequently, the United Kingdom has demonstrated strong motivation to see this export realized.
  • Contribution to NATO Capacity: All consortium members support the general argument that Türkiye’s NATO membership and this acquisition would strengthen the alliance’s collective defence and air power capacity.


Türkiye’s potential procurement of the Eurofighter Typhoon is not merely an inventory modernization issue but a complex geopolitical negotiation that reflects internal political dynamics within the European defence industry consortium and the limits of cooperation among NATO members.


Author Information

Avatar
AuthorArif Zahid YükselDecember 6, 2025 at 7:45 AM

Discussions

No Discussion Added Yet

Start discussion for "Eurofighter Typhoon" article

View Discussions

Contents

  • Foundations of the Development Program

  • Germany’s Withdrawal Attempt

  • Workshare Disputes and Production Contract

  • Cooperation Structure and Supply Mechanism

    • Management and Customer Interface (NETMA)

    • Industrial Consortium (Eurofighter GmbH)

  • Engine Cooperation (EUROJET) and Shares

  • Technical Specifications

    • Aerodynamics and Airframe Structure

    • Performance

  • Avionics and Sensing Systems

    • Radar Systems (Euroradar CAPTOR)

    • PIRATE IRST and Passive Sensing

    • Praetorian DASS and Electronic Warfare

    • Cockpit and Human-Machine Interface (HMI)

  • Weapon Systems and Operational Applications

    • Air-to-Air and Air-to-Ground Capabilities

    • Modernization Tranches

  • National Air Forces and Inventory Details

  • Combat Experience and Role

    • Strategic and Geopolitical Contribution

  • Türkiye’s Eurofighter Typhoon Procurement and Cooperation Context

    • Procurement Process and Agreement

    • Geopolitical Dimension of Cooperation and Consortium Approval

Ask to Küre