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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
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25:1
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gptkbp:controls
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digital control system
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gptkbp:cooling_system
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air-cooled
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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:durability
|
long durability
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gptkbp:elevation
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up to 15,000 m
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gptkbp:emissions_standard
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low emissions
variable area nozzle
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gptkbp:engine
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gptkb:RD-33
gptkb:advanced_technology
high performance
high reliability
ongoing research
electric starter
pylon-mounted
twin-engine configuration
dual-spool
continuous development
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gptkbp:engine_type
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turbofan
multiple variants
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gptkbp:fan_art
|
single-stage fan
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gptkbp:first_flight
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gptkb:1980s
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gptkbp:fuel_capacity
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3.5 m
1.1 m
1000 kg
high efficiency
3000 liters
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gptkbp:fuel_type
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annular
kerosene
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|
https://www.w3.org/2000/01/rdf-schema#label
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RD-33 MK-500
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gptkbp:introduced
|
2000s
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gptkbp:is_designed_for
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gptkb:Mikoyan_Mi_G-29
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gptkbp:is_tested_for
|
ground testing
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gptkbp:launch_date
|
30 seconds
|
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gptkbp:length
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3.5 m
|
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gptkbp:maintenance
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scheduled maintenance
100 hours
|
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gptkbp:manufacturer
|
Klimov
|
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gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:noise_level
|
low noise
|
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gptkbp:operational_range
|
long range
|
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gptkbp:origin
|
gptkb:Russia
|
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gptkbp:produced_by
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Klimov
|
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gptkbp:propulsion
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gptkb:battle
300 seconds
5:1
5000 kgf
|
|
gptkbp:services
|
up to 4000 hours
|
|
gptkbp:successor
|
gptkb:RD-33_M
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gptkbp:supports
|
90 kg/s
|
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gptkbp:surface
|
digital fly-by-wire
|
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gptkbp:type
|
afterburning turbofan engine
|
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gptkbp:used_in
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gptkb:Mi_G-29_K
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gptkbp:weight
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about 1000 kg
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gptkbp:bfsParent
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gptkb:RD-33_MK
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gptkbp:bfsLayer
|
6
|