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gptkbp:instance_of
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gptkb:jet_engine
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|
gptkbp:application
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gptkb:military_aircraft
|
|
gptkbp:bore
|
150 mm
|
|
gptkbp:compression_ratio
|
6.5:1
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gptkbp:configuration
|
V-type
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gptkbp:control_system
|
mechanical control
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gptkbp:cooling_system
|
liquid-cooled
water-cooled
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gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:displacement
|
42.5 L
|
|
gptkbp:engine
|
gptkb:military_aircraft
gptkb:advanced_technology
gptkb:Klimov_VK-105
gptkb:historical_context
gptkb:historical_significance
mass production
post-war development
electric starter
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gptkbp:engine_configuration
|
gptkb:V12
inline engine
front-mounted
detailed specifications
Klimov design
|
|
gptkbp:engine_power
|
high performance
high reliability
1,200 hp at 2,800 rpm
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|
gptkbp:engine_type
|
reciprocating engine
VK-107 A-1
|
|
gptkbp:first_flight
|
gptkb:1944
|
|
gptkbp:fuel_capacity
|
1,000 mm
800 mm
1,800 mm
|
|
gptkbp:fuel_economy
|
200 L/h
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-107 A
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:impact
|
impact on aviation
|
|
gptkbp:maintenance
|
moderate maintenance
|
|
gptkbp:manufacturer
|
Klimov
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|
gptkbp:max_speed
|
3,000 rpm
|
|
gptkbp:power_output
|
1,200 hp
|
|
gptkbp:production_years
|
1944-1947
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
Klimov VK-108
|
|
gptkbp:torque
|
2,000 Nm
2,000 Nm at 2,000 rpm
|
|
gptkbp:type
|
V12 piston engine
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:weight
|
450 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_VK-24_engine
gptkb:Klimov_VK-44_engine
gptkb:Klimov_VK-46_engine
|
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gptkbp:bfsLayer
|
8
|