Klimov M-105P V-12 liquid-cooled piston engine
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:configuration |
V-12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:displacement |
35 liters
|
| gptkbp:engineType |
V-12
|
| gptkbp:firstFlight |
1940s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| gptkbp:manufacturer |
gptkb:Klimov
|
| gptkbp:notableFeature |
cannon firing through propeller hub
|
| gptkbp:powerOutput |
1100 hp
|
| gptkbp:supercharger |
single-stage
|
| gptkbp:usedInAircraft |
gptkb:Yakovlev_Yak-7
gptkb:Yakovlev_Yak-1 gptkb:Yakovlev_Yak-9 gptkb:Petlyakov_Pe-2 gptkb:Lavochkin_LaGG-3 |
| gptkbp:valveConfiguration |
overhead camshaft
|
| gptkbp:bfsParent |
gptkb:Yakovlev_Yak-1
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Klimov M-105P V-12 liquid-cooled piston engine
|