|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
fighter aircraft
|
|
gptkbp:application
|
military aviation
|
|
gptkbp:climate
|
1,500 °C
|
|
gptkbp:compressionRatio
|
axial
|
|
gptkbp:controls
|
gptkb:FADEC_system
digital electronic control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:engine
|
twin-engine
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
RD-33MK
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:firstRace
|
1980
|
|
gptkbp:fuel_capacity
|
high
high thrust
0.85 kg/(kN·h)
|
|
gptkbp:fuelType
|
annular
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov RD-33
|
|
gptkbp:inspiration
|
gptkb:Rolls-Royce_RB.199
|
|
gptkbp:is_used_in
|
gptkb:Mikoyan_MiG-29
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:maximum_speed
|
Mach 2.25
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notableUsers
|
gptkb:Russian_Air_Force
|
|
gptkbp:number_of_stages
|
9
|
|
gptkbp:operational_status
|
1990s
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:origin
|
gptkb:Russia
|
|
gptkbp:performances
|
excellent
3,000 hours
|
|
gptkbp:productionYears
|
1970s to 1980s
|
|
gptkbp:propulsion
|
8,300 lbf
6.92
|
|
gptkbp:related_engine
|
Klimov RD-500
Brayton_cycle
RD_series
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
18,000 m
|
|
gptkbp:successor
|
gptkb:Klimov_RD-33MK
|
|
gptkbp:team
|
Klimov design bureau
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:weight
|
1,200 kg
|