|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:budget
|
high
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:competitors
|
gptkb:GE_F414
|
|
gptkbp:controls
|
gptkb:football_match
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country
|
multiple countries
|
|
gptkbp:design
|
4,000 hours
|
|
gptkbp:developer
|
1990s
high
|
|
gptkbp:diameter
|
1.0 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
low
variable geometry
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_test_facility
2
twin-engine
air start
pylon-mounted
|
|
gptkbp:engine_type
|
axial compressor
high-pressure turbine
dual-spool
|
|
gptkbp:family
|
gptkb:M53_engine_family
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_capacity
|
high
0.85 kg/k N/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
|
|
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:aircraft
|
|
gptkbp:max_speed
|
Mach 2.0
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_features
|
high thrust-to-weight ratio
|
|
gptkbp:operational_area
|
combat missions
|
|
gptkbp:operational_range
|
2,000 km
|
|
gptkbp:propulsion
|
6.0
optional
90 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:upgrades
|
gptkb:battle
|
|
gptkbp:used_in
|
gptkb:Eurofighter_Typhoon
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
|
|
gptkbp:bfsLayer
|
5
|