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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
|
annular combustion chamber
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gptkbp:compressor_type
|
axial compressor
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gptkbp:control_system
|
manual control system
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gptkbp:cooling_system
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air-cooled
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gptkbp:country_of_origin
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gptkb:Soviet_Union
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gptkbp:design
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designed by Klimov design bureau
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gptkbp:design_features
|
simple design features
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gptkbp:development
|
1950s
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gptkbp:diameter
|
0.9 m
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|
gptkbp:elevation
|
effective at high altitudes
|
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gptkbp:emissions_standard
|
high emissions
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gptkbp:engine
|
Brayton cycle
requires external starter
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gptkbp:engine_configuration
|
turbojet engine configuration
mounted on aircraft fuselage
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gptkbp:engine_power
|
limited operational life
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gptkbp:engine_type
|
several variants developed
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gptkbp:exported_to
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gptkb:various_countries
|
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gptkbp:first_flight
|
gptkb:1955
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|
gptkbp:fuel_economy
|
moderate fuel efficiency
high fuel consumption rate
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|
gptkbp:fuel_type
|
kerosene
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gptkbp:historical_significance
|
important in Soviet aviation history
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gptkbp:historical_use
|
used in Cold War era aircraft.
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-28 engine
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gptkbp:influenced_by
|
earlier Soviet jet engines
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gptkbp:is_tested_for
|
extensively tested before deployment
tested in various conditions
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gptkbp:legacy
|
influenced future jet engine designs
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gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
requires regular maintenance
|
|
gptkbp:manufacturer
|
Klimov
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|
gptkbp:material
|
made from high-strength alloys
|
|
gptkbp:noise_level
|
high noise level
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gptkbp:operational_history
|
used in various Soviet aircraft
|
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gptkbp:performance
|
high thrust-to-weight ratio
|
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gptkbp:production_years
|
produced from 1955 to 1970
|
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gptkbp:propulsion
|
no thrust vectoring
2800 lbf
|
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gptkbp:related_aircraft
|
compatible with multiple fighter jets
integrated into multiple aircraft models
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gptkbp:reliability
|
reliable engine
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gptkbp:replaced_by
|
gptkb:Klimov_VK-30_engine
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gptkbp:specification
|
detailed technical specifications available
|
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gptkbp:successor
|
gptkb:Klimov_VK-30
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gptkbp:turbine_type
|
single-stage turbine
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gptkbp:type
|
turbojet
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gptkbp:used_in
|
gptkb:Mikoyan_Mi_G-21
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gptkbp:weight
|
400 kg
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gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
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gptkbp:bfsLayer
|
7
|