Rolls-Royce Merlin Mk II or III
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.4 in (137 mm)
|
| gptkbp:compressionRatio |
6.0:1
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
27 litres
|
| gptkbp:engineType |
liquid-cooled V12 piston engine
|
| gptkbp:firstFlight |
1938
|
| gptkbp:fuelType |
100 octane aviation gasoline
carburettor |
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableFor |
used in early WWII British fighters
|
| gptkbp:powerOutput |
1,030 hp (768 kW)
|
| gptkbp:stroke |
6.0 in (152 mm)
|
| gptkbp:successor |
Rolls-Royce Merlin Mk XX
|
| gptkbp:supercharger |
single-stage
|
| gptkbp:usedInAircraft |
gptkb:aircraft
gptkb:Hawker_Hurricane |
| gptkbp:weight |
1,335 lb (606 kg)
|
| gptkbp:bfsParent |
gptkb:Hawker_Hurricane_Mk_I
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Merlin Mk II or III
|