Eurojet EJ200 (25331330967)
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The Eurojet EJ200 is a military
low-bypass turbofan The turbofan or fanjet is a type of airbreathing jet engine that is widely used in aircraft engine, aircraft propulsion. The word "turbofan" is a portmanteau of "turbine" and "fan": the ''turbo'' portion refers to a gas turbine engine which ac ...
used as the powerplant of the
Eurofighter Typhoon The Eurofighter Typhoon is a European multinational 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 ...
. The engine is largely based on the
Rolls-Royce Rolls-Royce (always hyphenated) may refer to: * Rolls-Royce Limited, a British manufacturer of cars and later aero engines, founded in 1906, now defunct Automobiles * Rolls-Royce Motor Cars, the current car manufacturing company incorporated in ...
XG-40 technology demonstrator, which was developed in the 1980s. The EJ200 is built by the
EuroJet Turbo GmbH EuroJet Turbo GmbH is a multi-national engine manufacturing consortium. It is headquartered in Hallbergmoos, Germany. The consortium was created in 1986 to manage the development, production, support, maintenance, support and sales of the EJ200, ...
consortium. The EJ200 is also used in the
Bloodhound LSR ''Bloodhound LSR'', formerly ''Bloodhound SSC'', is a British land vehicle designed to travel at supersonic speeds with the intention of setting a new world land speed record. The arrow-shaped car, under development since 2008, is powered by a je ...
supersonic land speed record attempting car.


Development


Rolls-Royce XG-40

Rolls-Royce began development of the XG-40 technology demonstrator engine in 1984. Development costs were met by the British government (85%) and Rolls-Royce. On 2 August 1985, Italy, West Germany and the UK agreed to go ahead with the Eurofighter. The announcement of this agreement confirmed that France had chosen not to proceed as a member of the project. One issue was French insistence that the aircraft be powered by the
SNECMA M88 The Snecma M88 is a French afterburning turbofan engine developed by Snecma (now known as Safran Aircraft Engines) for the Dassault Rafale fighter. History The program for the M88 arose from a need for a suitable propulsion system for air-supe ...
, in development at the same time as the XG-40.


Eurojet EJ200

The Eurojet consortium was formed in 1986 to co-ordinate and manage the project largely based on XG-40 technology. In common with the XG-40, the EJ200 has a three-stage fan with a high pressure ratio, five-stage low-aspect-ratio high-pressure (HP) compressor, a combustor using advanced cooling and thermal protection, and single-stage HP and LP turbines with powder metallurgy discs and
single crystal In materials science, a single crystal (or single-crystal solid or monocrystalline solid) is a material in which the crystal lattice of the entire sample is continuous and unbroken to the edges of the sample, with no grain boundaries.RIWD. "Re ...
blades. A reheat system (afterburner) provides thrust augmentation. The variable area final nozzle is a convergent-divergent design. In December 2006, Eurojet completed deliveries of the 363 EJ200s for the Tranche 1 Eurofighters. Tranche 2 aircraft require 519 EJ200s. , Eurojet was contracted to produce a total of 1,400 engines for the Eurofighter project.


HAL Tejas

In 2009, Eurojet entered a bid, in competition with General Electric's F414, to supply a thrust vectoring variant of the EJ200 to power the
HAL Tejas Mk2 HAL may refer to: Aviation * Halali Airport (IATA airport code: HAL) Halali, Oshikoto, Namibia * Hawaiian Airlines (ICAO airline code: HAL) * HAL Airport, Bangalore, India * Hindustan Aeronautics Limited an Indian aerospace manufacturer of fight ...
after both the indigenous Kaveri engine and the General Electric F404 used in prototypes and early production models proved to have insufficient performance. After evaluation and acceptance of the technical offer provided by both Eurojet and GE Aviation, the IAF preferred the EJ200 as it lighter and more compact but after the commercial quotes were compared in detail GE Aviation was declared as the lowest bidder. A second consideration by HAL was industrial offsets, if local Eurojet engine production was set up for the Tejas it would make future Eurofighter aircraft bids to India cheaper and more competitive with the Tejas whereas it was assumed the US would not allow aircraft using the engine to be sold to India, however October 2020 Boeing offered to sell F-18 aircraft to the Indian Navy.


TAI TFX

On 20 January 2015 ASELSAN of Turkey and Eurojet Turbo GmbH signed a Memorandum of Understanding to collaborate on the EJ200 military turbofan engine programme. It is envisaged that the collaboration would produce a derivative of the EJ200 with thrust vectoring for use in Turkey's TFX 5th generation air superiority fighter programme. Eurojet EJ200 is not selected for TFX program. TFX will use
General Electric F110 The General Electric F110 is an afterburning turbofan jet engine produced by GE Aviation. The engine is derived from the General Electric F101 and shares its core design, and primarily powers tactical fighter aircraft. The F118 is a non-afterb ...
engine until indigenous manufactured by TRMOTOR.


Landspeed record attempt

An EJ200 engine, together with a rocket engine, will power the
Bloodhound LSR ''Bloodhound LSR'', formerly ''Bloodhound SSC'', is a British land vehicle designed to travel at supersonic speeds with the intention of setting a new world land speed record. The arrow-shaped car, under development since 2008, is powered by a je ...
for an attempt at the land speed record. The target speed is at least 1000 mph."http://www.bloodhoundssc.com/fia-world-land-speed-record"


Variants


EJ2x0

Stage 1: * The EJ2x0 with 20% growth compared to the original EJ200. The EJ2x0 engine will have dry thrust increasing to some 72 kN (or 16,200 lbf) with a reheated output of around 103 kN (or 23,100 lbf). Stage 2: * The new engine plan to increase the output 30% more power compared to the original EJ200. The engine will have dry thrust of around 78 kN (or 17,500 lbf) with a reheated output of around 120 kN (or 27,000 lbf).


Applications

*
Eurofighter Typhoon The Eurofighter Typhoon is a European multinational 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 ...
*
Bloodhound LSR ''Bloodhound LSR'', formerly ''Bloodhound SSC'', is a British land vehicle designed to travel at supersonic speeds with the intention of setting a new world land speed record. The arrow-shaped car, under development since 2008, is powered by a je ...
*
Liquid fly-back booster Liquid Fly-back Booster (LFBB) was a German Aerospace Center's (DLR's) project concept to develop a liquid rocket booster capable of reusing for Ariane 5 in order to significantly reduce the high cost of space transportation and increase envir ...
(Cancelled)


Specifications (EJ200)


See also


References

;Notes ;Footnotes


External links


Eurojet GmbH

Rolls-Royce EJ200

EJ200 fact sheet

EUROJET Offers its EJ200 Engine for the Tejas, Indian Light Combat Aircraft
{{Joint development aeroengines Low-bypass turbofan engines 1990s turbofan engines Eurofighter Typhoon