Last site update: 03-10-2008

 

         

 

  

 

Eurofighter EF2000 Typhoon

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Eurofighter EF2000 Typhoon

The Eurofighter EF2000 Typhoon is a twin-engine swing role fighter with delta-wing and canards, designed and built by a four nations consortium consisting of British Aerospace (UK), Daimler-Benz Aerospace DASA (Germany), Alenia Aerospazio (Italy), and CASA (Spain).

Initial design of the Eurofighter began in 1986 by the three nations involved in the Tornado project (UK, Germany and Italy) who required an air superiority fighter to counter the next generation of Russian built fighters as the Mikoyan MiG-29 "Fulcrum" and the Sukhoi Su-27 "Flanker" then entering service. One key element of the design was maneuverability during close air combat.

The Eurofighter program began with a one-of prototype the EAP (Experimental Aircraft Program) a technology demonstrator built by British Aerospace with help from Germany to demonstrate some of the systems of the Eurofighter, including the carefree handling fly by wire system, multifunction cockpit-displays and direct voice input. The first flight of the EAP was on August 8, 1986 from BAe Warton with David Eagles in the cockpit. The EAP flew only 165 hours in five years.

The German Eurofighter 98+29 first flight was from DASA's home base Manching on March 27, 1994 with chief test pilot Peter Weger. It was a 45 minutes flight. The DA1 and DA2 flew the first part of the test flights with the Tornado engine, the Turbo-union RB199. The third prototype (Italian prototype) flew from the beginning with the Euro jet EJ200 turbofans.

The Typhoon incorporates several new state of the art aerial systems including the ECR-90 multirole radar built by companies from all four partner nations and IRIS-T an infra-red search and track weapon aiming system coupled with helmet mounted symbology. Other systems include a defensive Aids sub-system (DASS), wide-angle head up display and VTAS, a Voice Throttle and Stick control system that includes direct voice input of some commands and HOTAS (Hand on Throttle and Stick) to ease the pilots workload.

 

 

Developing Nations: United Kingdom, Italy, Germany and Spain.
Task: multi-role combat
First Flight: See the table futher down
Crew: 1 or two in two-seater/trainer
Wing Span: 10,50 m
Length: 14,50 m
Height: 4,0 m
Engine (s): Euro Jet EJ200-03Z (2x)
Weight: 9750 kg
Max.Take off weight: 21000 kg
Max. Speed: 2125 km/h
Max. Range:  
Weapons:

- Mauser 27 mm cannon

- AIM-120 AMRAAM

- FRAAM

- IRIS-T

- Paveway II

- Paveway III LGB

- Storm Shadow

 

Eurofighter Typhoon's test-fleet:

Type Registration Configuration Operator Manufacturer First flight
EAP ZF534 Single RAF British Aerospace Aug. 8, 1986
DA 1 98+29 Single Luftwaffe DASA March 27, 1994
DA 2 ZH588 Single RAF British Aerospace April 6, 1994
DA 3 MMX-602 Single AMI Alenia June 4, 1995
DA 4 ZH590 Dual RAF British Aerospace March 14, 1997
DA 5 98+30 Single Luftwaffe DASA Feb. 24, 1997
DA 6  XCE-16-01 Dual FAE CASA Aug. 31, 1996
DA 7 MMX-803 Single AMI Alenia Jan. 27, 1997
IPA1   Dual   British Aerospace  
IPA2   Dual   Alenia  
IPA3   Dual   DASA  
IPA4   Single   CASA  
IPA5   Single   British Aerospace  

 

        The 5 Instrumented Production Aircraft (IPA)

will be flying in the next configurations:

IPA1 

defensive aids sub-system integration
IPA2  air to surface weapon integration sensor fusion

IPA3

air to air weapon integration

IPA4

air to surface weapon integration and environmental trails

IPA5

Air to air and air to surface weapon integration

 

Order-book so far:
Austria 12
Germany 180
Greece 60 (postponed until after 2004)
Italy 121
Spain 87
UK 232

 

The NETMA (NATO Eurofighter and Tornado Management Agency) invited South Korea to join (as first non NATO country) the Eurofighter program, this to involve the Korean industry in the production of the Eurofighter.

 

 

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