Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bore |
4 in
|
| gptkbp:configuration |
V12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
867 cu in
|
| gptkbp:firstFlight |
1916
|
| gptkbp:fuelType |
petrol
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Falcon V12
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:numberBuilt |
2500
|
| gptkbp:powerOutput |
190-275 hp
|
| gptkbp:predecessor |
gptkb:Rolls-Royce_Hawk
|
| gptkbp:productionEndYear |
1927
|
| gptkbp:productionStartYear |
1916
|
| gptkbp:stroke |
5.5 in
|
| gptkbp:successor |
gptkb:Rolls-Royce_Eagle
|
| gptkbp:usedIn |
gptkb:Bristol_F.2_Fighter
gptkb:Airco_DH.4 gptkb:Sopwith_Cuckoo |
| gptkbp:valvetrain |
gptkb:SOHC
|
| gptkbp:bfsParent |
gptkb:Bristol_F.2_Fighter_(historic)
|
| gptkbp:bfsLayer |
6
|