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gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:aircraft
|
fighter jets
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:climate
|
900 °C
|
|
gptkbp:compressionRatio
|
8:1
|
|
gptkbp:controls
|
hydraulic control
|
|
gptkbp:coolingSystem
|
air
air-cooled
|
|
gptkbp:criticalReception
|
30 psi
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
high
|
|
gptkbp:engine
|
inline layout
KRD-600-1
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
centrifugal compressor
axial turbine
KRD-600A
|
|
gptkbp:exhaustSystem
|
straight exhaust
subsonic intake
|
|
gptkbp:firstFlight
|
1950s
|
|
gptkbp:fuel_capacity
|
moderate
0.8 kg/s
|
|
gptkbp:fuelType
|
spark ignition
kerosene
annular combustion chamber
dual fuel system
gear pump
|
|
gptkbp:future_plans
|
ground testing
|
|
gptkbp:historical_significance
|
early jet engine technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
KRD-600 turbojet engine
|
|
gptkbp:inspiration
|
high speed flight
|
|
gptkbp:launched
|
air start
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
KRD
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:number_of_stages
|
4
|
|
gptkbp:operational_status
|
1950s to 1970s
|
|
gptkbp:operationalRange
|
up to 12,000 m
|
|
gptkbp:productionYears
|
1940s to 1950s
|
|
gptkbp:propulsion
|
5:1
6000 lbf
|
|
gptkbp:regulatoryCompliance
|
ICAO_standards
|
|
gptkbp:related_engine
|
Brayton_cycle
KRD_series
|
|
gptkbp:services
|
2000 hours
|
|
gptkbp:successor
|
gptkb:KRD-700_turbojet_engine
|
|
gptkbp:weight
|
1200 kg
|