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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:aircraft_operated
|
military and civilian
heavy transport aircraft
|
|
gptkbp:application
|
cargo transport
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
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gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
30,000 hours
|
|
gptkbp:developer
|
1970s to 1980s
|
|
gptkbp:diameter
|
1,200 mm
1,300 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
twin-engine
pylon-mounted
D-18 family
|
|
gptkbp:engine_type
|
high bypass ratio
axial compressor
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_capacity
|
high efficiency
0.5 kg/k N·h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
high-pressure fuel system
|
|
gptkbp:horsepower
|
0.1 kg/k N
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
D-18 T turbofan
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:launch_site
|
electric starter
|
|
gptkbp:length
|
4,200 mm
|
|
gptkbp:maintenance
|
5,000 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
850 km/h
|
|
gptkbp:noise_level
|
low noise
advanced design
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:operational_range
|
over 5,000 km
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:propulsion
|
gptkb:battle
not equipped
18,000 kgf
|
|
gptkbp:services
|
gptkb:1985
|
|
gptkbp:supports
|
high airflow
|
|
gptkbp:type
|
dual-spool
|
|
gptkbp:used_in
|
gptkb:Antonov_An-124
|
|
gptkbp:weight
|
1,800 kg
|
|
gptkbp:bfsParent
|
gptkb:Mriya
|
|
gptkbp:bfsLayer
|
6
|