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gptkbp:instance_of
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gptkb:engine
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gptkbp:application
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gptkb:aircraft
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|
gptkbp:compression_ratio
|
25:1
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gptkbp:controls
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gptkb:full_authority_digital_engine_control_(FADEC)
advanced control system
digital electronic control system
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gptkbp:cooling_system
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air-cooled
effective cooling system
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gptkbp:developer
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gptkb:Monarch
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gptkbp:diameter
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1.1 m
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|
gptkbp:elevation
|
up to 15,000 m
|
|
gptkbp:emissions_standard
|
low emissions
variable area intake
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|
gptkbp:engine
|
high performance
high reliability
twin-spool
pylon-mounted
quick startup time
twin-spool turbofan
|
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gptkbp:engine_type
|
turbofan
afterburning turbofan engine
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gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:first_flight
|
gptkb:1990
|
|
gptkbp:fuel_capacity
|
3.5 m
1.1 m
800 kg
high fuel efficiency
low fuel consumption
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-33 MK-400
|
|
gptkbp:is_designed_for
|
gptkb:Mikoyan_Mi_G-29
|
|
gptkbp:launched
|
bleed air start
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
100 hours
easy maintenance
|
|
gptkbp:manufacturer
|
gptkb:United_Engine_Corporation
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:number_of_rooms
|
annular combustion chamber
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gptkbp:operational_area
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gptkb:aircraft
|
|
gptkbp:produced_by
|
Klimov
|
|
gptkbp:propulsion
|
gptkb:battle
300 seconds
5:1
4000 kgf
|
|
gptkbp:related_to
|
gptkb:Mikoyan_Mi_G-35
|
|
gptkbp:services
|
3000 hours
|
|
gptkbp:successor
|
gptkb:RD-33_MK-300
|
|
gptkbp:technology
|
supercruise
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:variant
|
gptkb:RD-33
|
|
gptkbp:weight
|
about 800 kg
|
|
gptkbp:bfsParent
|
gptkb:RD-33_MK
|
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gptkbp:bfsLayer
|
6
|