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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:air_support
|
40 lb/s
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
manual control
|
|
gptkbp:cooling_system
|
air-cooled
air cooling
|
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:design_date
|
1945
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Derwent
fighter jets
Brayton cycle
air start
developed during WWII
produced in large numbers
influenced future jet engines
important in jet engine development.
upgraded to VK-1 F
|
|
gptkbp:engine_configuration
|
axial-flow
detailed specifications available
reverse flow design
|
|
gptkbp:engine_power
|
good performance at altitude
moderate fuel efficiency
moderate reliability
|
|
gptkbp:engine_type
|
VK-1 A
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_economy
|
0.85 lb/lbf·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-1
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
gptkb:Moscow
ground testing required
|
|
gptkbp:length
|
3.4 m
|
|
gptkbp:maintenance
|
periodic maintenance required
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
1,100 km/h
|
|
gptkbp:noise_level
|
high noise level
|
|
gptkbp:notable_users
|
gptkb:Soviet_Air_Force
|
|
gptkbp:operational_history
|
gptkb:Korean_War
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:propulsion
|
1.5
no thrust vectoring
1,800 lbf
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1_F
|
|
gptkbp:turbine_type
|
single spool
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Mikoyan-Gurevich_Mi_G-15
gptkb:Mi_G-15
gptkb:Mi_G-15bis
|
|
gptkbp:bfsLayer
|
5
|