Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
4.5 in
|
| gptkbp:compressionRatio |
4.9:1
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
20.3 L
|
| gptkbp:engineType |
liquid-cooled V12 piston engine
|
| gptkbp:firstFlight |
1917
|
| gptkbp:fuelType |
gptkb:carburetor
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableEvent |
powered the first non-stop transatlantic flight
|
| gptkbp:notableMission |
gptkb:Alcock_and_Brown's_1919_transatlantic_flight
|
| gptkbp:numberBuilt |
over 3000
|
| gptkbp:powerOutput |
350 hp
|
| gptkbp:stroke |
6.5 in
|
| gptkbp:usedInAircraft |
gptkb:Handley_Page_O/400
gptkb:Vickers_Vimy gptkb:Airco_DH.4 |
| gptkbp:valvetrain |
gptkb:SOHC
|
| gptkbp:weight |
847 lb (dry)
|
| gptkbp:bfsParent |
gptkb:Vickers_Vimy
|
| gptkbp:bfsLayer |
6
|
| http://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Eagle VIII
|