General (Allgemeine Angaben)
The operational requirements for Eurofighter Typhoon were agreed by the Chiefs of Air Staff of Germany, Italy, Spain and the United Kingdom in the form of a European Staff Requirement which was re-affirmed in January 1994.
The agreement, the basis for the project's development programme, defined the requirement for an extremely agile fighter that will dominate the skies to the mid-21st Century - a single seat, twin-engine fighter with optimal performance in Beyond Visual Range (BVR) and close combat, with significant ground attack capabilities.
Eurofighter Typhoon offers maximum operational effectiveness and flexibility, high survivability, extensive technological growth potential, as well as high reliability and maintainability with low operating costs.
Industrial consortia set up as part of the Project include:
- Eurofighter GmbH, set up to manage the development and production of the complete weapon system. It is owned by the four Eurofighter Partner Companies (EPC), with agreed development work shares:
BAE Systems (BAES - UK) 33 %
Alenia Aeronautica (ALN - Italy) 21 %
EADS Deutschland (Germany) 33 %
EADS CASA (Spain) 13 %
Performance/Mass (Flugleistungen und Massen):
Two Eurojet EJ200 turbofan engines, each delivering 60kN (13,490lb) in dry power and 90kN (20,250lb) with reheat (Antrieb zwei Eurojet EJ 200 mit Nachbrenner, Schub 60 kN)
Maximum speed of Mach 2.0 (Maximalgeschwindigkeit)
Runway requirement (Startbahnlänge) of 700m (2,300ft)
g limits +9/-3
Basic Mass Empty (Leermasse) 10,995kg (24,239lb)
Normal maximum take-off mass (Startmasse) 23,500kg (50,700lb)
Dimensions (Abmessungen)
Wing span (Spannweite) 10.95m (35ft 11in)
Wing aspect ratio 2.2
Overall length (Länge) 15.96m (52ft 4in)
Overall height (Höhe) 5.28m (17 ft 4 in)
Wing area 50.0sq m (538sq ft)
Weapons and stores (Bewaffnung und Beladung):
Internally mounted 27mm Mauser cannon (innen montierte 27mm Mauser Kanone)
Total of 13 external stores stations: five (incl. one optional wet) under fuselage and four (incl. one optional wet) under each wing
Four BVRAAM underfuselage in semi-conformal carriage configuration
Mix of Beyond Visual Range Air-to-Air missiles (BVRAAM) and Short-Range Air-to-Air Missiles (SRAAM) carried externally
Full range of Air-to-Surface weaponry including:
Laser guided bombs; Advanced anti armour weapons;Conventionally armed stand-off missiles
4 Mittelstrecken-Luft/Luft-Flugkörper (Meteor, AMRAAM) 2 Kurzstrecken-Luft/Luft-Flugkörper (IRIS-T, ASRAAM) zur Selbstverteidigung sowie bis zu 6 lasergelenkten Bomben beladen werden
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