Eurojet EJ200

GPTKB entity

Statements (55)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:military_aircraft
gptkbp:average_temperature high temperature
gptkbp:bypass_ratio gptkb:3.0
gptkbp:certification certified for military use
gptkbp:combustor_type annular
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
gptkbp:cooling_system air-cooled
gptkbp:country_of_origin gptkb:Germany
gptkbp:design 6,000 hours
gptkbp:diameter 1.0 m
gptkbp:emissions_standard low emissions
gptkbp:engine Brayton cycle
joint development by multiple countries.
gptkbp:engine_configuration twin-spool
gptkbp:engine_power high performance
gptkbp:engine_type turbofan
EJ200-30, EJ200-40
gptkbp:fan_art single-stage fan
gptkbp:fuel_capacity 1,200 kg
1.0 m
3.8 m
gptkbp:fuel_economy high efficiency
0.85 kg/k N/h
gptkbp:fuel_type gptkb:Jet_A-1
gptkbp:gearbox reduction gearbox
gptkbp:has_programs gptkb:Eurofighter_program
https://www.w3.org/2000/01/rdf-schema#label Eurojet EJ200
gptkbp:is_tested_for extensive testing
gptkbp:length 3.8 m
gptkbp:maintenance 1,500 hours
gptkbp:manufacturer gptkb:Eurojet_Turbo_Gmb_H
gptkbp:noise_level low
gptkbp:number_of_stages gptkb:3
gptkbp:operational_range 0 to 50,000 ft
gptkbp:operational_status in service
gptkbp:original_run gptkb:1997
gptkbp:produced_by gptkb:Eurojet_Turbo_Gmb_H
gptkbp:propulsion no
90 k N
gptkbp:related_aircraft Eurofighter Typhoon, Saab JAS 39 Gripen
gptkbp:service_entry gptkb:2003
gptkbp:startup_type air-start
gptkbp:turbine_type high-pressure turbine
gptkbp:type afterburning turbofan
gptkbp:type_of gptkb:turbofan_engine
gptkbp:used_in gptkb:Eurofighter_Typhoon
gptkbp:video_output axial
gptkbp:weight 1,200 kg
gptkbp:bfsParent gptkb:Airbus_Eurofighter_Typhoon
gptkb:Snecma_M88
gptkb:Eurofighter_Typhoon
gptkb:Typhoon_fighter
gptkbp:bfsLayer 5