Rolls-Royce Kestrel IIS V-12
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
60-degree V-12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
21 L
|
| gptkbp:engineType |
V-12
|
| gptkbp:firstFlight |
1927
|
| gptkbp:fuelType |
petrol
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Kestrel IIS V-12
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:powerOutput |
approximately 600 hp
|
| gptkbp:successor |
gptkb:Rolls-Royce_Merlin
|
| gptkbp:supercharger |
yes
|
| gptkbp:usedDuring |
interwar period
|
| gptkbp:usedIn |
gptkb:Hawker_Fury
gptkb:Hawker_Hart gptkb:Supermarine_Southampton |
| gptkbp:valvetrain |
DOHC
|
| gptkbp:bfsParent |
gptkb:Hawker_Osprey
|
| gptkbp:bfsLayer |
7
|