Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
20.3 L
|
| gptkbp:engineType |
V12 piston engine
|
| gptkbp:firstFlight |
1915
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableFor |
first Rolls-Royce aero engine to enter production
powered first non-stop transatlantic flight |
| gptkbp:notableMission |
gptkb:Alcock_and_Brown_transatlantic_crossing
|
| gptkbp:numberBuilt |
4,681
|
| gptkbp:powerOutput |
225 hp to 360 hp
|
| gptkbp:predecessor |
none
|
| gptkbp:productionStartYear |
1915–1928
|
| gptkbp:successor |
gptkb:Rolls-Royce_Condor
|
| gptkbp:usedDuring |
gptkb:World_War_I
|
| gptkbp:usedIn |
gptkb:Felixstowe_F.2A
gptkb:Handley_Page_O/400 gptkb:Vickers_Vimy gptkb:Airco_DH.4 |
| gptkbp:bfsParent |
gptkb:Vickers_Vimy_aircraft
gptkb:Rolls-Royce_Limited gptkb:Airco_DH.4 gptkb:Airco_DH.4_(historic) gptkb:Vickers_Vimy_(historic) |
| gptkbp:bfsLayer |
6
|
| http://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Eagle
|