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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:military_aircraft
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gptkbp:combustor_type
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annular combustion chamber
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gptkbp:compression_ratio
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6.5:1
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gptkbp:control_system
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manual control
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gptkbp:cooling_system
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air-cooled
air cooling
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gptkbp:country_of_origin
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gptkb:Soviet_Union
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gptkbp:diameter
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1.1 m
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gptkbp:engine
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modular design
air start
influenced future designs
produced in large numbers
innovative for its time
jet propulsion technology
developed in the late 1940s
1950s technology
afterburner option available
part of Soviet aviation history
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gptkbp:engine_configuration
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axial flow
Klimov design
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gptkbp:engine_power
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reliable engine
high thrust-to-weight ratio
moderate efficiency
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gptkbp:engine_specifications
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detailed specifications available
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gptkbp:engine_type
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gptkb:jet_engine
gptkb:VK-18_F
used in various aircraft models
compatible with Mi G-15
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gptkbp:first_flight
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1947
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gptkbp:fuel_type
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kerosene
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https://www.w3.org/2000/01/rdf-schema#label
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Klimov VK-18 engine
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gptkbp:impact
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significant impact on aviation
influenced jet engine design.
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gptkbp:is_tested_for
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extensively tested
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gptkbp:length
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3.5 m
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gptkbp:maintenance
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periodic maintenance required
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gptkbp:manufacturer
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Klimov
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gptkbp:noise_level
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high noise level
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gptkbp:number_of_stages
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gptkb:5
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gptkbp:operational_use
|
1950s
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gptkbp:power_output
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2,200 k W
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gptkbp:propulsion
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3,000 lbf
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gptkbp:replaced_by
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gptkb:Klimov_VK-1_engine
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gptkbp:successor
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gptkb:Klimov_VK-1_engine
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gptkbp:type
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gptkb:turbofan_engine
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gptkbp:used_in
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gptkb:Mikoyan-Gurevich_Mi_G-15
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gptkbp:weight
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1,200 lb
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gptkbp:bfsParent
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gptkb:Klimov_design_bureau
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gptkbp:bfsLayer
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7
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