Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:configuration |
V-12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:engineType |
V12 liquid-cooled piston engine
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Klimov
|
| gptkbp:notableFeature |
increased power output over VK-105PA
|
| gptkbp:powerOutput |
1,240 hp
|
| gptkbp:predecessor |
gptkb:Klimov_VK-105
|
| gptkbp:successor |
gptkb:Klimov_VK-107
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedInAircraft |
gptkb:Yakovlev_Yak-7
gptkb:Yakovlev_Yak-1 gptkb:Yakovlev_Yak-9 gptkb:Lavochkin_LaGG-3 |
| gptkbp:valveConfiguration |
overhead camshaft
|
| gptkbp:bfsParent |
gptkb:Klimov_M-105P
gptkb:Klimov_M-105_V-12_liquid-cooled_piston_engine gptkb:Yak-9D gptkb:Yak-9K gptkb:Yak-9T |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Klimov VK-105PF
|