|
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 throttle
|
|
gptkbp:cooling_system
|
liquid cooling
liquid-cooled
water-cooled
|
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:displacement
|
38 liters
|
|
gptkbp:engine
|
advanced engineering techniques
post-World War II
limited production
developed in the 1940s
electric starter
production challenges
dual ignition system
influenced future designs
various Soviet aircraft
|
|
gptkbp:engine_configuration
|
aerodynamic design
V-12
military specifications
cradle mount
|
|
gptkbp:engine_legacy_impact
|
significant impact on aviation
|
|
gptkbp:engine_power
|
high reliability
high power-to-weight ratio
moderate efficiency
linear power curve
|
|
gptkbp:engine_type
|
gptkb:VK-38_A
reciprocating engine
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_economy
|
high fuel consumption
|
|
gptkbp:fuel_type
|
gptkb:carburetor
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-38 engine
|
|
gptkbp:ignition_system
|
magneto
|
|
gptkbp:intended_use
|
gptkb:fighter_aircraft
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:maintenance
|
periodic inspections
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
3,000 rpm
|
|
gptkbp:number_of_engines
|
gptkb:12
|
|
gptkbp:power_output
|
1,200 hp
|
|
gptkbp:production_years
|
1947-1950
|
|
gptkbp:successor
|
gptkb:Klimov_VK-105
|
|
gptkbp:torque
|
flat torque curve
2,000 Nm
|
|
gptkbp:type
|
V-12 piston engine
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:valve_configuration
|
DOHC
|
|
gptkbp:weight
|
450 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|