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gptkbp:instanceOf
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turbojet engine
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|
gptkbp:aircraft
|
gptkb:Mikoyan-Gurevich_MiG-19
gptkb:Mikoyan-Gurevich_MiG-15
gptkb:Mikoyan-Gurevich_MiG-17
improved performance
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|
gptkbp:application
|
military aircraft
|
|
gptkbp:climate
|
up to 1,000 °C
|
|
gptkbp:compressionRatio
|
6:1
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|
gptkbp:controls
|
manual control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
compact design
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|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engineConfiguration
|
single-spool
|
|
gptkbp:engineType
|
several variants
axial-flow engine
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuel_capacity
|
moderate fuel efficiency
0.85 kg/kN·h
2,000 kg/h
|
|
gptkbp:fuelType
|
spark plug
kerosene
annular combustor
|
|
gptkbp:hasArea
|
extensive testing
|
|
gptkbp:historical_significance
|
important in aviation history
|
|
gptkbp:historicalEvent
|
derived from RD-500
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NE-20 turbojet engine
|
|
gptkbp:influence
|
influenced future designs
|
|
gptkbp:launchSite
|
air starter
|
|
gptkbp:legacy
|
legacy in jet engine technology
|
|
gptkbp:length
|
3.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:NPO_Saturn
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:number_of_stages
|
5
|
|
gptkbp:operational_status
|
gptkb:Cold_War
|
|
gptkbp:operationalHistory
|
gptkb:Soviet_Union
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:performances
|
1,000 hours
|
|
gptkbp:predecessor
|
RD-500 engine
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:productionYears
|
1955-1965
|
|
gptkbp:propulsion
|
0.1
20 kN
|
|
gptkbp:related_engine
|
NPO_Saturn_engines
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:retirementYear
|
retired in the 1970s
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:successor
|
RD-500 engine
|
|
gptkbp:team
|
gptkb:Mikoyan_design_bureau
|
|
gptkbp:weight
|
200 kg
|