|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:fighter_aircraft
|
|
gptkbp:average_temperature
|
900 ° C
|
|
gptkbp:combustor_type
|
axial flow
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:control_system
|
manual control
|
|
gptkbp:cooling_system
|
air-cooled
air-cooled system
|
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:design_date
|
1945
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
gptkb:military_aircraft
modular design
post-war era
Brayton cycle
afterburner
developed in 1940s
45 k N thrust
|
|
gptkbp:engine_configuration
|
gptkb:turbofan_engine
gptkb:classified_information
high thrust
single spool
|
|
gptkbp:engine_power
|
average
decent
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:VK-45_F
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_economy
|
moderate
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-45 engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notable_users
|
gptkb:Soviet_Air_Force
|
|
gptkbp:operational_history
|
used in 1950s
|
|
gptkbp:propulsion
|
0.112
45 k N
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:weight
|
400 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|