|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
Mikoyan_family
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:compressionRatio
|
18:1
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
|
gptkbp:design
|
2000 hours
|
|
gptkbp:designedBy
|
gptkb:Mikoyan
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:displacement
|
not applicable
|
|
gptkbp:emissionsStandard
|
high
|
|
gptkbp:energyEfficiency
|
moderate
|
|
gptkbp:engine
|
3.8 m
800 kg
pylon-mounted
D-30 family
|
|
gptkbp:engineConfiguration
|
single-spool
|
|
gptkbp:engineDisplacement
|
1.1 m
|
|
gptkbp:enginePower
|
80 kN
|
|
gptkbp:engineType
|
turbojet engine
|
|
gptkbp:firstAwarded
|
1960
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:firstHeld
|
1990s
|
|
gptkbp:fuelCapacity
|
0.8 kg/kN/h
|
|
gptkbp:fuelType
|
spark plug
kerosene
annular combustion chamber
|
|
gptkbp:hasDepartment
|
yes
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
D-30 engine
|
|
gptkbp:launchDate
|
30 seconds
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:maxSpeed
|
Mach_2.5
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notableFeature
|
D-30F,_D-30KP
|
|
gptkbp:numberBuilt
|
over 10,000
|
|
gptkbp:operationalRange
|
varies by aircraft
|
|
gptkbp:operationalStatus
|
high
up to 15,000 m
|
|
gptkbp:propulsion
|
0.1
no
80 kN
|
|
gptkbp:relatedPatent
|
RD-500
|
|
gptkbp:reliability
|
moderate
|
|
gptkbp:replacedBy
|
D-30F
|
|
gptkbp:services
|
1960
|
|
gptkbp:successor
|
D-30F
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:usedIn
|
gptkb:Mikoyan_MiG-21
gptkb:Mikoyan_MiG-23
|
|
gptkbp:weight
|
about 800 kg
|