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
|