|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:category
|
piston engine
military aircraft engine
Soviet invention
|
|
gptkbp:combustors
|
annular
|
|
gptkbp:compressionRatio
|
3-stage fan, 9-stage axial compressor
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
1.040 m
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
aviation kerosene
|
|
gptkbp:hasTower
|
2-stage high-pressure, 1-stage low-pressure
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov RD-33 turbofan
|
|
gptkbp:introduced
|
1980
|
|
gptkbp:length
|
4.229 m
|
|
gptkbp:manufacturer
|
gptkb:Klimov
|
|
gptkbp:notableVariant
|
RD-33 Series 3
RD-33B
RD-33MK
RD-93
SMR-95
|
|
gptkbp:primaryUser
|
gptkb:Russian_Air_Force
gptkb:Indian_Air_Force
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:relatedTo
|
gptkb:Klimov_RD-93
SMR-95
|
|
gptkbp:status
|
in service
|
|
gptkbp:thrust
|
50 kN
81.4 kN
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:usedInAircraft
|
gptkb:Mikoyan_MiG-35
gptkb:Mikoyan_MiG-29
HAL Tejas (prototype)
Shenyang J-31
|
|
gptkbp:weight
|
1055 kg
|
|
gptkbp:bfsParent
|
gptkb:Mikoyan_MiG-29
|
|
gptkbp:bfsLayer
|
6
|