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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
|
|
gptkbp:controls
|
digital control system
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|
gptkbp:cooling_system
|
air-cooled
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gptkbp:designed_by
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gptkb:Moscow_Institute_of_Thermal_Technology
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gptkbp:developer
|
5 years
|
|
gptkbp:diameter
|
1,000 mm
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|
gptkbp:elevation
|
up to 15,000 m
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|
gptkbp:emissions_standard
|
low
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|
gptkbp:engine
|
gptkb:RD-500
gptkb:RD-33_MK
brayton cycle
RD-33 M-1
RD-33 M-2
RD-33 M-3
|
|
gptkbp:engine_type
|
axial compressor
two-stage turbine
|
|
gptkbp:exported_to
|
gptkb:India
gptkb:Kazakhstan
gptkb:Malaysia
gptkb:Politician
gptkb:Serbia
|
|
gptkbp:first_flight
|
gptkb:1983
|
|
gptkbp:fuel_capacity
|
2,000 kg/h
|
|
gptkbp:fuel_type
|
kerosene
annular combustion chamber
variable area
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-33 M
|
|
gptkbp:investment
|
3.5 M Pa
|
|
gptkbp:launched
|
air start
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:production_years
|
gptkb:1984
|
|
gptkbp:propulsion
|
gptkb:battle
300 seconds
6.75
81 k N
85 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
1,500 hours
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:used_in
|
gptkb:Mikoyan_Mi_G-29_M
gptkb:Mikoyan_Mi_G-29
|
|
gptkbp:variant
|
RD-33, RD-33 MK
|
|
gptkbp:weight
|
about 1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:RD-33_MK-500
|
|
gptkbp:bfsLayer
|
7
|