|
gptkbp:instanceOf
|
aircraft engine
|
|
gptkbp:bore
|
130 mm
|
|
gptkbp:compressionRatio
|
6.5:1
|
|
gptkbp:coolingSystem
|
liquid-cooled
water-cooled
|
|
gptkbp:displacement
|
27.0 L
|
|
gptkbp:drivetrain
|
overhead valves
|
|
gptkbp:engine
|
low
800 mm
military aircraft
1,200 mm
advanced for its time
influenced future designs
|
|
gptkbp:engineConfiguration
|
gptkb:V-12
|
|
gptkbp:enginePower
|
450 hp at 2,400 rpm
0.9 hp/L
|
|
gptkbp:engineType
|
piston engine
Kestrel_II,_Kestrel_III,_Kestrel_IV,_Kestrel_V
|
|
gptkbp:firstFlight
|
1920
|
|
gptkbp:fuel_capacity
|
0.4 kg/hp/hr
|
|
gptkbp:fuelType
|
Champion
aviation gasoline
magneto
|
|
gptkbp:hasArea
|
British_Civil_Airworthiness_Authority
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Kestrel VI
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Fury
gptkb:Bristol_F.2_Fighter
Gloster Gladiator
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:noise_level
|
moderate
|
|
gptkbp:performances
|
high
periodic inspections
1,500 hours
|
|
gptkbp:powerOutput
|
450 hp
|
|
gptkbp:productionYears
|
1920-1935
|
|
gptkbp:setting
|
V engine
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Merlin
|
|
gptkbp:torque
|
1,200 Nm
|
|
gptkbp:tuning
|
naturally aspirated
|
|
gptkbp:type
|
gptkb:V-12_engine
|
|
gptkbp:weight
|
250 kg
|