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gptkbp:instance_of
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gptkb:jet_engine
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|
gptkbp:application
|
gptkb:military_aircraft
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|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:certification
|
JAA certification
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|
gptkbp:combustor_type
|
annular combustion chamber
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|
gptkbp:compressor_type
|
axial compressor
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|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
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gptkbp:design_purpose
|
gptkb:fighter_aircraft
|
|
gptkbp:development
|
gptkb:1980s
|
|
gptkbp:diameter
|
1.0 m
1.1 m
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
M-60 engine
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_economy
|
high fuel efficiency
0.85 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
integrated gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M-701 engine
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:number_of_stages
|
5 stages
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:propulsion
|
no
approximately 18,000 lbf
|
|
gptkbp:related_aircraft
|
Mitsubishi F-2 A
Mitsubishi F-2 A/ B
Mitsubishi F-2 A/ B fighter
Mitsubishi F-2 B
Mitsubishi F-2 fighter
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service
|
approximately 4,000 hours
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Mitsubishi_F-2
|
|
gptkbp:weight
|
approximately 1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:L-29_M
gptkb:Soko_J-20_Kraguj
|
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gptkbp:bfsLayer
|
7
|