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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:aircraft_type
|
gptkb:fighter_aircraft
|
|
gptkbp:application
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gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular combustion chamber
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:development
|
joint development
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:elevation
|
up to 15,000 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:RB199
Brayton cycle
developed in the 1970s
air start
possible upgrades
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
detailed specifications available.
|
|
gptkbp:engine_type
|
gptkb:M53-P36_A
|
|
gptkbp:first_flight
|
gptkb:1979
|
|
gptkbp:fuel_economy
|
high
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M53-P36 engine
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:MTU_Aero_Engines
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:power_output
|
12,000 lbf
|
|
gptkbp:propulsion
|
no
90 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1980
|
|
gptkbp:successor
|
M53-P2 engine
|
|
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
|