|
gptkbp:instanceOf
|
Aircraft engine
|
|
gptkbp:application
|
Military aircraft
|
|
gptkbp:bore
|
150 mm
|
|
gptkbp:compressionRatio
|
6.5:1
|
|
gptkbp:controls
|
Throttle_control
|
|
gptkbp:coolingSystem
|
Liquid-cooled
|
|
gptkbp:cylinderCount
|
12
|
|
gptkbp:displacement
|
41.5 L
|
|
gptkbp:engine
|
600 kg
V engine
Electric starter
Fuselage-mounted
Liquid cooling system
V-12, liquid-cooled engine specifications.
|
|
gptkbp:engineConfiguration
|
V-12 configuration
|
|
gptkbp:engineDisplacement
|
Developed_during_World_War_II
|
|
gptkbp:engineType
|
gptkb:Piston_engine
High performance for its time
Routine maintenance required
ASh-82F,_ASh-82FN
|
|
gptkbp:firstFlight
|
1940
|
|
gptkbp:fuelCapacity
|
250 L/h
|
|
gptkbp:fuelType
|
Avgas
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
ASh-82W
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:notableUsers
|
gptkb:Soviet_Air_Force
|
|
gptkbp:operationalHistory
|
Used_extensively_in_Soviet_aircraft
|
|
gptkbp:powerOutput
|
1,600 hp
|
|
gptkbp:propulsion
|
Variable-pitch propeller
2.67 hp/kg
|
|
gptkbp:relatedPatent
|
ASh-82F,_ASh-82FN
|
|
gptkbp:setting
|
gptkb:V-12
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:ASh-82F
|
|
gptkbp:torque
|
1,200 Nm
|
|
gptkbp:type
|
gptkb:V-12_piston_engine
|
|
gptkbp:usedIn
|
Il-2 Sturmovik
|
|
gptkbp:weight
|
600 kg
|
|
gptkbp:yearEstablished
|
1940
|