This article was automatically translated from the original Turkish version.
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First Flight / Entry into Service | 27 March 1994, 4 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 certain 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 (Germany, Spain), BAE Systems (United Kingdom), Leonardo (Italy) | ||||||||
Maximum Altitude | 19812 metres (65000 ft) | ||||||||
Maneuverability | Canard-delta wing, aerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system | ||||||||
Electronic Warfare (EW) | Praetorian DASS (Electronic Support Measures, ECM, Deployable Radar Jammer) | ||||||||
Engine | 2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium) | ||||||||
Maximum Thrust | Each engine with afterburner produces 90 kN (20000 lbf) | ||||||||
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 layered challenges including Cold War dynamics, national budget constraints, and complex international workshare negotiations. Although initially designed as an air superiority fighter, extensive modernization programs (Tranches) implemented during its operational service 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.

Eurofighter Typhoon (TonyNojmanSK)
The foundations of the Eurofighter program were laid in 1979 with the launch of the European Combat Aircraft (ECF) studies by France, the United Kingdom, and West Germany. These efforts evolved in 1983 into the Future European Fighter Aircraft (FEFA) program, involving France, the United Kingdom, Germany, Italy, and Spain. However, deep disagreements emerged in later stages regarding aircraft design requirements. France advocated for a lighter, single-engine platform suitable for carrier operations (eventually 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 countries united under the European Fighter Aircraft (EFA) program. The program’s technology demonstrator, the British Aerospace EAP (Experimental Aircraft Programme), made its first flight in 1986 and established the canard-delta configuration for the EFA. The first EFA prototype (DA1) flew in 1994, and the aircraft was officially named Typhoon in 1998.
Eurofighter Typhoon (Haci Productions)
During the program’s development phase, Germany faced significant pressure in the early 1990s due to the heavy financial burden of reunification. Chancellor Helmut Kohl pledged to cancel the Eurofighter project, while Defense Minister Volker Rühe proposed in early 1991 that Germany withdraw from the program and adopt 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 importantly, binding and penal contractual agreements signed among the partner governments, prevented Germany from unilaterally exiting. This penalty system established by Rühe’s predecessors proved decisive in ensuring the program’s continuation despite Kohl’s political will.

Eurofighter Typhoon (Joe Ambrogio)
In 1995, new tensions emerged over workshare balances due to changes in order quantities. When Eurofighter was established, workshare was allocated according to initial order proportions: United Kingdom 33%, Germany 33%, Italy 21%, and Spain 13%.
However, as all countries reduced their initial order quantities (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 new shares should have been UK 39%, Germany 24%, Italy 22%, and Spain 15%. Germany resisted such a significant loss of workshare.
After lengthy 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 revised 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.
The Eurofighter Typhoon program is structured around two main management bodies and four primary industrial partners.

Eurofighter Typhoon (Rafael Minguet Delgado)
The aircraft’s heart, the EJ200 turbofan engines, are developed and produced by a separate consortium: EUROJET Turbo GmbH.
This cooperation model ensures that all partners benefit economically, even in large procurements such as Germany’s Tranche 5 order, by requiring hundreds of new engine supply contracts to be signed between EUROJET and NETMA.
The Eurofighter Typhoon is a fourth-generation and beyond (4.5-generation) fighter aircraft integrating innovative solutions in avionics, aerodynamics, and materials technology.
The Typhoon employs a canard and delta wing configuration to achieve superior maneuverability at high angles of attack and supersonic speeds. This aerodynamic design intentionally 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.
EJ200, Eurofighter Typhoon Rolls-Royce (MechDesignTV)
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.
PIRATE IRST (Passive Infrared Search and Track System) is located on the left side of the nose. Its passive operation reduces the aircraft’s risk of detection by avoiding electromagnetic emissions, while enabling long-range target detection and tracking. PIRATE can be used in air-to-air (multi-target tracking) and air-to-ground (target identification/lock-on) roles and provides infrared imaging for visual identification.
Praetorian DASS (Defensive Aids Sub-System) was developed by the EuroDASS consortium.
The cockpit is designed to maximize pilot situational awareness and control capability and includes:

Eurofighter Typhoon (Aviation Station)
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 true “swing-role” platform through integration of modern munitions.
The aircraft’s service life and capabilities are managed through incremental production and modernization tranches:
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.
Eurofighter Typhoon Weapons (Aviation Station)
The Typhoon is currently operated by nine different air forces: the United Kingdom, Germany, Italy, Spain, Austria, Saudi Arabia, Oman, Kuwait and Qatar.
Since entering operational service in 2003, the aircraft has participated in various international operations and demonstrated its multirole capabilities:
The Typhoon enables user nations to guarantee sovereignty over their own airspace while serving as a flexible and reliable platform for international interventions and NATO missions. Its continuous modernization ensures user nations remain technologically current and maintain interoperability with other allied platforms, such as the F-35, in international operations.

Türkiye’s interest in procuring the Eurofighter Typhoon is part of its broader effort to modernize its air power, particularly following uncertainties arising from the F-35 program.
Türkiye has initiated official discussions with the United Kingdom regarding the procurement of up to 40 Typhoon fighter aircraft. The first major step in this process was the signing of a Memorandum of Understanding (MoU) in 2025 between the defense ministries of the United Kingdom and Türkiye. This constitutes an official preliminary step in the procurement process.
The Typhoon is a platform requiring the full export approval of all four consortium countries (UK, Germany, Italy, Spain). Türkiye’s procurement process has clearly revealed the industrial and geopolitical complexity of the program:
Türkiye’s potential procurement of the Eurofighter Typhoon is not merely an inventory modernization issue, but a complex geopolitical negotiation process reflecting internal political dynamics within the European defense industry consortium and the limits of cooperation among NATO members.

Eurofighter Typhoon (Muhammet Emir Şeker)
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First Flight / Entry into Service | 27 March 1994, 4 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 certain 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 (Germany, Spain), BAE Systems (United Kingdom), Leonardo (Italy) | ||||||||
Maximum Altitude | 19812 metres (65000 ft) | ||||||||
Maneuverability | Canard-delta wing, aerodynamically unstable design and Quadruple-Redundant Fly-by-Wire (FBW) control system | ||||||||
Electronic Warfare (EW) | Praetorian DASS (Electronic Support Measures, ECM, Deployable Radar Jammer) | ||||||||
Engine | 2 x Eurojet EJ200 Turbofan (produced by the EUROJET Consortium) | ||||||||
Maximum Thrust | Each engine with afterburner produces 90 kN (20000 lbf) | ||||||||
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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 Contributions
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 Ground Attack 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