|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Tupolev_Tu-16
gptkb:Mikoyan-Gurevich_Mi_G-17
gptkb:Ilyushin_Il-28
gptkb:Mikoyan-Gurevich_Mi_G-15
gptkb:Mikoyan-Gurevich_Mi_G-19
gptkb:Tupolev_Tu-4
|
|
gptkbp:application
|
gptkb:fighter_aircraft
|
|
gptkbp:certification
|
Soviet certification
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
manual control
|
|
gptkbp:cooling_system
|
air-cooled
air cooling
|
|
gptkbp:design_date
|
1945
|
|
gptkbp:development
|
1945-1947
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:engine
|
gptkb:VK-42_M
mass production
500 hours
Brayton cycle
simple design
air start
early jet engine development.
|
|
gptkbp:engine_afterburner
|
no
|
|
gptkbp:engine_combustion_efficiency
|
high
|
|
gptkbp:engine_configuration
|
gptkb:Mikhail_Klimov
single spool
|
|
gptkbp:engine_power
|
good
moderate
2000 hours
|
|
gptkbp:engine_type
|
gptkb:VK-42_F
jet propulsion
|
|
gptkbp:exhaust_system
|
straight exhaust
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_economy
|
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
gravity feed
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-42 engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
4.2 m
|
|
gptkbp:maintenance
|
moderate
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:operational_history
|
used in 1950s
|
|
gptkbp:operational_use
|
gptkb:Soviet_Air_Force
|
|
gptkbp:propulsion
|
no
10:1
10 k N/kg
8000 lbf
|
|
gptkbp:replaced_by
|
gptkb:Klimov_VK-1
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1
|
|
gptkbp:turbine_type
|
axial
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|