|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:fighter_aircraft
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:combustion_chamber_pressure
|
6.5 MPa
|
|
gptkbp:control_system
|
digital electronic control system
|
|
gptkbp:cooling_system
|
air-cooled
effective cooling system
|
|
gptkbp:designed_by
|
Klimov
|
|
gptkbp:development
|
1970s to 1980s
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
gptkb:RD-33_family
military applications
air start
dual-spool
various upgrades available
advanced features included
rich history in aviation.
|
|
gptkbp:engine_configuration
|
twin-engine
modern design principles
detailed specifications available
81 k N with afterburner
|
|
gptkbp:engine_power
|
high performance
high reliability
up to 3,000 hours
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
multiple variants exist
|
|
gptkbp:exhaust_system
|
convergent-divergent
|
|
gptkbp:first_flight
|
gptkb:1983
|
|
gptkbp:fuel_economy
|
good fuel efficiency
2,000 kg/h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-33-4
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:is_tested_for
|
extensive testing conducted
|
|
gptkbp:length
|
3.2 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:operational_use
|
gptkb:Soviet_Air_Force
|
|
gptkbp:propulsion
|
no
0.27
81 k N
|
|
gptkbp:related_aircraft
|
Mi G-29, Mi G-35
|
|
gptkbp:specific_impulse
|
290 s
|
|
gptkbp:successor
|
gptkb:RD-33_MK
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Mikoyan_Mi_G-29
|
|
gptkbp:variant
|
gptkb:RD-33-3
|
|
gptkbp:weight
|
300 kg
|
|
gptkbp:bfsParent
|
gptkb:RD-33_series
|
|
gptkbp:bfsLayer
|
8
|