Top Document: rec.aviation.military Frequently Asked Questions (part 1 of 5) Previous Document: B.4. Dassault Rafale Next Document: B.6. JAST See reader questions & answers on this topic! - Help others by sharing your knowledge In 1982 British Aerospace began development of what was then called ACA (Agile Combat Aircraft), a fighter technology demonstrator, originally privately funded, although it later attracted some assistance from the British government. The single aircraft first flew on 8 August 1986, by which time it had been redesignated EAP (Experimental Aircraft Programme). Meanwhile, in December 1983, the air forces of France, Germany (then West Germany), Italy, Spain, and the UK announced a programme for the development of a next generation combat aircraft, designated FEFA (Future European Fighter Aircraft), based largely on the EAP demonstrator, and on similar work done by MBB (now part of DASA) in Germany, under the designation JF-90 (a research project rather than an actual aircraft). FEFA was originally intended to enter service with all five countries in the mid-1990s. From the beginning the programme was dogged by political, commercial, technological, and military infighting (leading _Flight International_ columnist Roger Bacon to suggest that the acronym actually stood for Five Europeans Farting Around). Disagreement over the size of the aircraft and the production schedule led France to withdraw from the programme in July 1985 (France wanted a smaller aircraft, and postponement of production to avoid competing with Dassault's Mirage 2000). In June 1986 Eurofighter GmbH was formed to manage what was now the EFA (European Fighter Aircraft) programme, with participation by British Aerospace (33%), MBB (now DASA, 33%), Aeritalia (now Alenia, 21%), and CASA (13%). The aircraft is now known as the Eurofighter 2000; a proper name is expected to be assigned eventually. The first flight was made on 27 March 1994; production delivery is expected to begin in 2000. Orders are 250 for the UK (but they're considering an increase to 350), 165 for Italy, 100 for Spain, and probably about 100-120 for Germany (who originally wanted 140 but are expected to reduce their order). BAe and Rolls-Royce have proposed a future version with VTOL capability. Vital statistics (Eurofighter 2000): length 14.50 m, span 10.50 m, empty weight 9750 kg, max weight 17000 kg, max speed 1912 km/h (Mach 1.8), ferry range 1112 km; power plant: two 90.00 kN augmented turbofans; armament: 27mm cannon, AAM rail on each wingtip, 11 hardpoints; max external load 6500 kg. User Contributions:Top Document: rec.aviation.military Frequently Asked Questions (part 1 of 5) Previous Document: B.4. Dassault Rafale Next Document: B.6. JAST Part1 - Part2 - Part3 - Part4 - Part5 - Single Page [ Usenet FAQs | Web FAQs | Documents | RFC Index ] Send corrections/additions to the FAQ Maintainer: avfaq@meanmach.actrix.gen.nz
Last Update March 27 2014 @ 02:11 PM
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