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gptkbp:instance_of
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gptkb:Team_Rocket
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gptkbp:aircraft_operated
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gptkb:fighter_aircraft
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gptkbp:application
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gptkb:military_aircraft
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
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gptkbp:cooling_system
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air-cooled
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gptkbp:design_features
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advanced design features
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gptkbp:design_purpose
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improved performance over RD-33
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gptkbp:designed_by
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gptkb:Kuznetsov_Design_Bureau
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gptkbp:development
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1990s
Kuznetsov engineers
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gptkbp:diameter
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1.1 m
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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
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gptkbp:engine
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gptkb:RD-33
dual-spool
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gptkbp:engine_configuration
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twin-engine configuration
inline layout
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gptkbp:exhaust_system
|
variable area
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gptkbp:exported_to
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export variants available
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gptkbp:first_flight
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gptkb:1999
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gptkbp:fuel_economy
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high fuel efficiency
efficient fuel consumption
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gptkbp:fuel_type
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kerosene
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gptkbp:history
|
derived from RD-33 engine
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|
https://www.w3.org/2000/01/rdf-schema#label
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RD-93
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gptkbp:is_tested_for
|
extensively tested
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gptkbp:launch_date
|
quick startup time
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gptkbp:length
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3.2 m
|
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gptkbp:maintenance
|
low maintenance requirements
|
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gptkbp:manufacturer
|
gptkb:Kuznetsov
|
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gptkbp:noise_level
|
low noise level
|
|
gptkbp:number_of_rooms
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single chamber
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|
gptkbp:operational_range
|
long operational range
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:operational_use
|
exported to several countries
|
|
gptkbp:performance
|
high performance
|
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gptkbp:propulsion
|
0.5
0.2
no thrust vectoring
81 k N
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gptkbp:related_aircraft
|
compatible with various aircraft
|
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gptkbp:reliability
|
high reliability
|
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gptkbp:service
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long service life
|
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gptkbp:specific_impulse
|
300 seconds
|
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gptkbp:type
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afterburning turbofan
|
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gptkbp:used_in
|
gptkb:Mikoyan_Mi_G-29_M
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gptkbp:weight
|
about 400 kg
|
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gptkbp:bfsParent
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gptkb:JF-17_Thunder
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gptkbp:bfsLayer
|
6
|