|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:budget
|
high
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:competitors
|
gptkb:GE_F414
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
4,000 hours
|
|
gptkbp:development
|
1990s
|
|
gptkbp:development_cost
|
high
|
|
gptkbp:diameter
|
1.0 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
air start
|
|
gptkbp:engine_configuration
|
twin-engine
pylon-mounted
|
|
gptkbp:engine_test_facility
|
gptkb:Rolls-Royce_test_facility
|
|
gptkbp:engine_type
|
dual-spool
|
|
gptkbp:exhaust_system
|
variable geometry
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_economy
|
high
0.85 kg/k N/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:has_family
|
gptkb:M53_engine_family
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M53-P35 engine
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
gptkb:military_aircraft
|
|
gptkbp:max_speed
|
Mach 2.0
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_features
|
high thrust-to-weight ratio
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_range
|
2,000 km
|
|
gptkbp:operational_use
|
combat missions
|
|
gptkbp:propulsion
|
6.0
optional
90 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:upgrades
|
yes
|
|
gptkbp:used_in
|
gptkb:Eurofighter_Typhoon
|
|
gptkbp:user_countries
|
multiple countries
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
|
|
gptkbp:bfsLayer
|
6
|