gptkbp:instance_of
|
gptkb:jet_engine
|
gptkbp:application
|
gptkb:military_aircraft
|
gptkbp:compression_ratio
|
6.5:1
|
gptkbp:configuration
|
V engine
|
gptkbp:control_system
|
mechanical control
|
gptkbp:cooling_system
|
liquid cooling
liquid-cooled
water-cooled
|
gptkbp:displacement
|
44 liters
|
gptkbp:engine
|
gptkb:Klimov_VK_engine_family
no
four-stroke
electric starter
Klimov
|
gptkbp:engine_configuration
|
inline engine
V-type engine
V-layout
cradle mount
|
gptkbp:engine_displacement
|
44 liters
|
gptkbp:engine_material
|
aluminum alloy
|
gptkbp:engine_power
|
1500 hp
2500 rpm
1100 k W
|
gptkbp:engine_type
|
reciprocating engine
VK-44
|
gptkbp:engine_volume
|
44 L
|
gptkbp:first_flight
|
1947
|
gptkbp:fuel_capacity
|
1.8 m
900 kg
1.2 m
1.0 m
|
gptkbp:fuel_type
|
aviation gasoline
high-octane gasoline
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-44 engine
|
gptkbp:ignition_system
|
spark ignition
|
gptkbp:manufacturer
|
Klimov
|
gptkbp:max_speed
|
2800 rpm
|
gptkbp:notable_users
|
gptkb:Soviet_Air_Force
|
gptkbp:number_of_engines
|
gptkb:12
|
gptkbp:power_output
|
1500 hp
|
gptkbp:production_years
|
1947-1950
|
gptkbp:propeller
|
variable-pitch propeller
|
gptkbp:replaced_by
|
gptkb:Klimov_VK-107_A
|
gptkbp:successor
|
gptkb:Klimov_VK-107
|
gptkbp:torque
|
3000 Nm
4000 Nm
|
gptkbp:type
|
V-12 engine
|
gptkbp:used_in
|
gptkb:Tupolev_Tu-4
|
gptkbp:valve_configuration
|
overhead valve
|
gptkbp:weight
|
800 kg
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
gptkbp:bfsLayer
|
7
|