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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:certification
|
Soviet certification
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
mechanical control
|
|
gptkbp:cooling_system
|
air-cooled
direct air cooling
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:engine
|
gptkb:Mikulin_AM-5
gptkb:Rolls-Royce_Derwent
gptkb:General_Electric_J47
1950-1955
modular design
Brayton cycle
air start
first Soviet turbojet engine
VK-1 F upgrade
|
|
gptkbp:engine_afterburner
|
no afterburner
|
|
gptkbp:engine_configuration
|
single-spool
Klimov design team
|
|
gptkbp:engine_inlet_type
|
subsonic inlet
|
|
gptkbp:engine_power
|
high reliability
1,500 hours
good performance
moderate efficiency
|
|
gptkbp:engine_production_quantity
|
over 10,000 units
|
|
gptkbp:exhaust_system
|
straight exhaust
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_economy
|
2,000 kg/h
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-1 F engine
|
|
gptkbp:is_tested_for
|
gptkb:Moscow
|
|
gptkbp:length
|
3,200 mm
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
1,100 km/h
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_history
|
used in Soviet aircraft
|
|
gptkbp:propulsion
|
6.67
8,000 lbf
no thrust vectoring
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1
|
|
gptkbp:turbine_type
|
axial turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:variant
|
VK-1 A
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:year_established
|
1950
|
|
gptkbp:bfsParent
|
gptkb:Klimov_VK-8_engine
|
|
gptkbp:bfsLayer
|
8
|