Eurofighter Jagdflugzeug GmbH

Eurofighter Typhoon

The Eurofighter Typhoon is a twin‑engine, multirole combat aircraft developed through a pan‑European collaboration led by Eurofighter Jagdflugzeug GmbH. Work began in the early 1980s when the United Kingdom, Germany, Italy and Spain launched the Future European Fighter Aircraft (FEFA) programme to replace aging fleets and achieve joint technological independence. The prototype first flew in 1994 and operational service entered in 2003, with the type now serving over a dozen air forces worldwide.

Key features include a highly agile delta wing and close‑coupled canard layout that delivers superb maneuverability at supersonic speeds, and a digital fly‑by‑wire control system that integrates advanced avionics. Powered by two EJ200 turbofan engines, the Typhoon can exceed Mach 2 and maintain high thrust‑to‑weight ratios. Its sensor suite combines an AESA radar, infrared search and track system, and data‑fusion capabilities, allowing seamless air‑to‑air and air‑to‑ground missions. The aircraft’s modular design supports continuous upgrades, keeping it relevant against evolving threats.

In aviation history the Eurofighter Typhoon represents a benchmark in multinational defense cooperation, delivering a modern, versatile platform that balances air superiority with strike capability, and it sets a standard for future European fighter development.

Dimensions

Wing Area
50 square metre
Length
15.96 metre
Height
5.28 metre
Mass
23400 kilogram

Performance

Service Ceiling
16765 metre
Range
1389 kilometre

Production & History

Units Produced
926
First Flight
1994
Service Entry
2003

Design & Classification

Manufacturer
Eurofighter Jagdflugzeug GmbH
Engine
Eurojet EJ200
Operator
Royal Saudi Air Force Royal Air Force of Oman Spanish Air and Space Force Austrian Air Force Italian Air Force Royal Air Force German Air Force
Wikidata ID
Q151384

External References