|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:bore
|
150 mm
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:configuration
|
V-type
|
|
gptkbp:cooling_system
|
liquid-cooled
water-cooled
|
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:displacement
|
43.5 L
|
|
gptkbp:engine
|
gptkb:fighter_aircraft
1947-1950
developed in 1940s
used in post-war aircraft.
|
|
gptkbp:engine_configuration
|
gptkb:V12
V-configuration
cradle mount
|
|
gptkbp:engine_intake
|
dual intake
|
|
gptkbp:engine_power
|
high reliability
high altitude performance
1,500 hp at 2,500 rpm
|
|
gptkbp:engine_type
|
gptkb:VK-43_A
reciprocating engine
|
|
gptkbp:exhaust_system
|
gptkb:exhaust_system
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_capacity
|
800 mm
1,500 mm
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-43 engine
|
|
gptkbp:ignition_system
|
magneto
|
|
gptkbp:maintenance
|
moderate maintenance
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:notable_users
|
gptkb:Soviet_Air_Force
|
|
gptkbp:number_of_engines
|
gptkb:12
|
|
gptkbp:power_output
|
1,500 hp
|
|
gptkbp:replaced_by
|
gptkb:Klimov_VK-105
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:Klimov_VK-105
|
|
gptkbp:torque
|
dry sump
2,000 Nm
|
|
gptkbp:type
|
V12 piston engine
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:weight
|
600 kg
|
|
gptkbp:year_established
|
1947
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|