Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:steam_locomotive
|
| gptkbp:bore |
5 in
|
| gptkbp:compressionRatio |
6.3:1
|
| gptkbp:configuration |
V-12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:developedBy |
gptkb:Liberty_L-12_aircraft_engine
|
| gptkbp:displacement |
1648 cu in
|
| gptkbp:firstProduced |
1941
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Liberty V-12 tank
|
| gptkbp:manufacturer |
gptkb:United_States
|
| gptkbp:notableUser |
gptkb:U.S._Army
|
| gptkbp:numberOfEngines |
12
|
| gptkbp:origin |
gptkb:United_States
|
| gptkbp:powerOutput |
340 hp
|
| gptkbp:stroke |
7 in
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedIn |
gptkb:M3_Lee
gptkb:M4_Sherman |
| gptkbp:valvetrain |
single overhead camshaft
|
| gptkbp:weight |
1,410 lb
|
| gptkbp:bfsParent |
gptkb:Liberty_L-12
|
| gptkbp:bfsLayer |
6
|