фото: RAF Eurofighter

Robert Sullivan • 23-01-2019  

Описание: The Eurofighter "Typhoon" is a twin-engine, canard–delta wing, multirole fighter. The "Typhoon" was designed originally as an air superiority fighter and is manufactured by a consortium of Airbus, BAE Systems and Leonardo that conducts the majority of the project through a joint holding company, Eurofighter Jagdflugzeug GmbH formed in 1986. NATO Eurofighter and "Tornado" Management Agency manages the project and is the prime customer. The aircraft's development effectively began in 1983 with the Future European Fighter Aircraft programme, a multinational collaboration among the UK, Germany, France, Italy and Spain. Disagreements over design authority and operational requirements led France to leave the consortium to develop the Dassault "Rafale" independently. A technology demonstration aircraft, the British Aerospace EAP, first took flight on 6 August 1986; the first prototype of the finalised Eurofighter made its first flight on 27 March 1994. The aircraft's name, "Typhoon", was adopted in September 1998; the first production contracts were also signed that year. Political issues in the partner nations significantly protracted the "Typhoon's" development: the sudden end of the Cold War, reduced European demand for fighter aircraft, and the debate over the aircraft's cost and work share. The "Typhoon" entered operational service in 2003; it has entered service with the air forces of Austria, Italy, Germany, the United Kingdom, Spain and Saudi Arabia. The air forces of Oman, Kuwait and Qatar are export customers, bringing the procurement total to 623 aircraft as of 2019. The Eurofighter "Typhoon" is a highly agile aircraft, designed to be a supremely effective dogfighter in combat. Later production aircraft have been increasingly better equipped to undertake air-to-surface strike missions and to be compatible with an increasing number of different armaments and equipment, including 'Storm Shadow' and the RAF's Brimstone'. The "Typhoon" had its combat debut during the 2011 military intervention in Libya with the UK's Royal Air Force and the Italian Air Force, performing aerial reconnaissance and ground-strike missions. The type has also taken primary responsibility for air-defence duties for the majority of customer nations. Development Origins The UK had identified a requirement for a new fighter as early as 1971. The AST 403 specification, issued by the Air staff in 1972, led to the P.96 conventional "tailed" design presented in the late 1970s. While the design would have met the Air Staff's requirements, the UK air industry had reservations, as it appeared to be very similar to the McDonnell Douglas F/A-18 "Hornet", which was then well advanced in its development. The P.96 design had little potential for growth, and when it entered production, it would secure few exports in a market in which the "Hornet" would be well established. However, the simultaneous West German requirement for a new fighter had led by 1979 to the development of the TKF-90 concept. This was a cranked delta wing design with forward close-coupled-canard controls and artificial stability. Although the British Aerospace designers rejected some of its advanced features such as engine vectoring nozzles and vented trailing edge controls, a form of boundary layer control, they agreed with the overall configuration. In 1979, Messerschmitt-B"olkow-Blohm (MBB) and British Aerospace (BAe) presented a formal proposal to their respective governments for the ECF, the European Collaborative Fighter or European Combat Fighter. In October 1979 Dassault joined the ECF team for a tri-national study, which became known as the European Combat Aircraft. It was at this stage of development the Eurofighter name was first attached to the aircraft. The development of different national prototypes continued. France produced the ACX. The UK produced two designs; the P.106 was a single-engined "lightweight" fighter, superficially resembling the JAS 39 "Gripen", the P.110 was a twin-engined fighter. The RAF rejected the P.106 concept on the grounds it had "half the effectiveness of the two-engined aircraft at two-thirds of the cost". West Germany continued to refine the TKF-90 concept. The ECA project collapsed in 1981 for several reasons, including differing requirements, Dassault's insistence on "design leadership" and the British preference for a new version of the RB199 to power the aircraft versus the French preference for the new Snecma M88. Consequently, the Panavia partners (MBB, BAe and Aeritalia) launched the Agile Combat Aircraft (ACA) programme in April 1982. The ACA was very similar to the BAe P.110, having a cranked delta wing, canards and a twin tail. One major external difference was the replacement of the side-mounted engine intakes with a chin intake. The ACA was to be powered by a modified version of the RB199. The German and Italian governments withdrew funding, and the UK Ministry of Defence agreed to fund 50% of the cost with the remaining 50% to be provided by industry. MBB and Aeritalia signed up with the aim of producing two aircraft, one at Warton and one by MBB. In May 1983, BAe announced a contract with the MoD for the development and production of an ACA demonstrator, the Experimental Aircraft Programme. In 1983 Italy, Germany, France, the UK and Spain launched the "Future European Fighter Aircraft" (FEFA) programme. The aircraft was to have short take off and landing (STOL) and beyond visual range (BVR) capabilities. In 1984, France reiterated its requirement for a carrier-capable version and demanded a leading role. Italy, West Germany and the UK opted out and established a new EFA programme. In Turin on 2 August 1985, West Germany, the UK and Italy agreed to go ahead with the Eurofighter; and confirmed France, along with Spain, had chosen not to proceed as a member of the project. Despite pressure from France, Spain rejoined the Eurofighter project in early September 1985. France officially withdrew from the project to pursue its own ACX project, which was to become the Dassault Rafale. By 1986, the programme's cost had reached lb180 million. When the EAP programme had started, the cost was supposed to be equally shared by government and industry, but the West German and Italian governments wavered on the agreement and the three main industrial partners had to provide lb100 million to keep the programme from ending. In April 1986, the BAe EAP was rolled out at BAe Warton, by this time also partially funded by MBB, BAe and Aeritalia. The EAP first flew on 6 August 1986. The Eurofighter bears a strong resemblance to the EAP. Design work continued over the next five years using data from the EAP. Initial requirements were: UK: 250 aircraft, Germany: 250, Italy: 165 and Spain: 100. The share of the production work was divided among the countries in proportion to their projected procurement – DASA (33%), British Aerospace (33%), Aeritalia (21%), and Construcciones Aeron'auticas SA (CASA) (13%). The Munich-based Eurofighter Jagdflugzeug GmbH was established in 1986 to manage development of the project and EuroJet Turbo GmbH, the alliance of Rolls-Royce, MTU Aero Engines, FiatAvio (now Avio) and ITP for development of the EJ200. The aircraft was known as Eurofighter EFA from the late 1980s until it was renamed EF 2000 in 1992. By 1990, the selection of the aircraft's radar had become a major stumbling-block. The UK, Italy and Spain supported the Ferranti Defence Systems-led ECR-90, while Germany preferred the APG-65-based MSD2000 (a collaboration between Hughes, AEG and GEC-Marconi). An agreement was reached after UK Defence Secretary Tom King assured his West German counterpart Gerhard Stoltenberg that the British government would approve the project and allow the GEC subsidiary Marconi Electronic Systems to acquire Ferranti Defence Systems from its parent, the Ferranti Group, which was in financial and legal difficulties. GEC thus withdrew its support for the MSD2000. Delays The financial burdens placed on Germany by reunification caused Helmut Kohl to make an election promise to cancel the Eurofighter. In early to mid-1991 German Defence Minister Volker R"uhe sought to withdraw Germany from the project in favour of using Eurofighter technology in a cheaper, lighter plane. Because of the amount of money already spent on development, the number of jobs dependent on the project, and the binding commitments on each partner government, Helmut Kohl was unable to withdraw; "R"uhe's predecessors had locked themselves into the project by a punitive penalty system of their own devising." In 1995 concerns over workshare appeared. Since the formation of Eurofighter the workshare split had been agreed at 33/33/21/13 (United Kingdom/Germany/Italy/Spain) based on the number of units being ordered by each contributing nation, all the nations then reduced their orders. The UK cut its orders from 250 to 232, Germany from 250 to 140, Italy from 165 to 121 and Spain from 100 to 87. According to these order levels the workshare split should have been 39/24/22/15 UK/Germany/Italy/Spain, however Germany was unwilling to give up such a large amount of work. In January 1996, after much negotiation between German and UK partners, a compromise was reached whereby Germany would purchase another 40 aircraft. The workshare split was 43% for EADS MAS in Germany and Spain; 37.5% BAE Systems in the UK; and 19.5% for Alenia in Italy. The next major milestone came at the Farnborough Airshow in September 1996. The UK announced the funding for the construction phase of the project. In November 1996 Spain confirmed its order but Germany delayed its decision. After much diplomatic activity between Germany and the UK, an interim funding arrangement of DM100 million (€51 million) was contributed by the German government in July 1997 to continue flight trials. Further negotiations finally resulted in Germany's approval to purchase the Eurofighter in October 1997. Testing The maiden flight of the Eurofighter prototype took place in Bavaria on 27 March 1994, flown by DASA chief test pilot Peter Weger. On 9 December 2004, Eurofighter "Typhoon" IPA4 began three months of Cold Environmental Trials (CET) at the Vidsel Air Base in Sweden, the purpose of which was to verify the operational behaviour of the aircraft and its systems in temperatures between -25 and 31 °C. The maiden flight of Instrumented Production Aircraft 7 (IPA7), the first fully equipped Tranche 2 aircraft, took place from EADS' Manching airfield on 16 January 2008. Procurement, production and costs The first production contract was signed on 30 January 1998 between Eurofighter GmbH, Eurojet and NETMA. The procurement totals were as follows: the UK 232, Germany 180, Italy 121, and Spain 87. Production was again allotted according to procurement: British Aerospace (37.42%), DASA (29.03%), Aeritalia (19.52%), and CASA (14.03%). On 2 September 1998, a naming ceremony was held at Farnborough, United Kingdom. This saw the Typhoon name formally adopted, initially for export aircraft only. The name continues the storm theme started by the Panavia "Tornado". This was reportedly resisted by Germany, perhaps because the Hawker "Typhoon" was a fighter-bomber aircraft used by the RAF during the Second World War to attack German targets. The name "Spitfire II" (after the famous British Second World War fighter, the Supermarine "Spitfire") had also been considered and rejected for the same reason early in the development programme. In September 1998, contracts were signed for production of 148 Tranche 1 aircraft and procurement of long lead-time items for Tranche 2 aircraft. In March 2008, the final aircraft out of Tranche 1 was delivered to the German Air Force, with all successive deliveries being at the Tranche 2 standard. On 21 October 2008, the first two of 91 Tranche 2 aircraft, ordered four years before, were delivered to RAF Coningsby. In October 2008, the Eurofighter nations were considering splitting the 236-fighter Tranche 3 into two parts. In June 2009, RAF Air Chief Marshal Sir Glenn Torpy suggested that the RAF fleet could be 123 jets, instead of the 232 previously planned. In spite of this reduction in required aircraft, on 14 May 2009 British Prime Minister Gordon Brown confirmed the UK would move ahead with the third batch purchase. A contract for the first part, Tranche 3A, was signed at the end of July 2009 for 112 aircraft split across the four partner nations, including 40 aircraft for the UK, 31 for Germany, 21 for Italy and 20 for Spain. These 40 aircraft were said to have fully covered the UK's obligations in the project by Air Commodore Chris Bushell, because of cost overruns in the project. The Eurofighter "Typhoon" is unique in modern combat aircraft in that there are four separate assembly lines. Each partner company assembles its own national aircraft, but builds the same parts for all aircraft (including exports); Premium AEROTEC (main centre fuselage), EADS CASA (right wing, leading edge slats), BAE Systems (front fuselage (including foreplanes), canopy, dorsal spine, tail fin, inboard flaperons, rear fuselage section) and Leonardo (left wing, outboard flaperons, rear fuselage sections). Production is divided into three tranches (see table below). Tranches are a production/funding distinction, and do not imply an incremental increase in capability with each tranche. Tranche 3 are based on late Tranche 2 aircraft with improvements added. Tranche 3 was split into A and B parts. Tranches were further divided up into production standard/capability blocks and funding/procurement batches, though these did not coincide, and are not the same thing; e.g., the Eurofighter designated FGR4 by the RAF is a Tranche 1, block 5. Batch 1 covered block 1, but batch 2 covered blocks 2, 2B and 5. On 25 May 2011 the 100th production aircraft, ZK315, rolled off the production line at Warton.

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