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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
digital control system
|
|
gptkbp:cooling_system
|
gptkb:Interpol
air-cooled
|
|
gptkbp:design
|
4,000 hours
|
|
gptkbp:development
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:disassembly
|
easy maintenance
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:RB199
modular design
mass production
developed in the 1970s
air start
performance upgrades available
|
|
gptkbp:engine_configuration
|
twin-engine
pylon-mounted
detailed specifications available.
|
|
gptkbp:engine_power
|
optimized for supersonic flight
|
|
gptkbp:engine_type
|
M53-P50 A
|
|
gptkbp:exhaust_system
|
variable geometry
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1979
|
|
gptkbp:fuel_economy
|
high
0.85 kg/k N/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M53-P50 engine
|
|
gptkbp:is_tested_for
|
ground testing
Rolls-Royce facility
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:propulsion
|
no
90 k N
110 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1982
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Panavia_Tornado
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
|
|
gptkbp:bfsLayer
|
6
|