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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:compressor_type
|
axial
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|
gptkbp:control_system
|
gptkb:manual
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|
gptkbp:cooling_system
|
air-cooled
air cooling
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gptkbp:country_of_origin
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gptkb:Soviet_Union
|
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gptkbp:design_date
|
1945
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gptkbp:development
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gptkb:Klimov_design_bureau
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gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissions_standard
|
low emissions
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gptkbp:engine
|
gptkb:fighter_aircraft
Brayton cycle
electric start
produced in large numbers
important in early jet aviation.
used in various Soviet aircraft
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gptkbp:engine_configuration
|
twin-shaft
3,000 lbf at sea level
VK-33-1
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|
gptkbp:engine_design_feature
|
compact design
|
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gptkbp:engine_overhaul_period
|
200 hours
|
|
gptkbp:engine_power
|
4.5 out of 5
1,000 hours
good performance at altitude
moderate fuel efficiency
|
|
gptkbp:engine_type
|
VK-33 A
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|
gptkbp:engine_weight_to_thrust_ratio
|
0.4
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_capacity
|
3.5 m x 0.9 m
|
|
gptkbp:fuel_economy
|
0.8 kg/s
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-33 engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
gptkb:Moscow
ground testing completed
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
Klimov
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|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_history
|
used in the Korean War
|
|
gptkbp:propulsion
|
2.5
3,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Mikoyan-Gurevich_Mi_G-17
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1
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|
gptkbp:turbine_type
|
single spool
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|