|
gptkbp:instanceOf
|
Aircraft engine
|
|
gptkbp:application
|
Military aviation
|
|
gptkbp:compressionRatio
|
6.5:1
|
|
gptkbp:coolingSystem
|
Liquid-cooled
|
|
gptkbp:cylinderCount
|
24
|
|
gptkbp:displacement
|
24.0 L
24,000 cc
Significant_in_WWII_aviation.
|
|
gptkbp:emissionsStandard
|
Turbocharged
|
|
gptkbp:engine
|
Moderate
Innovative
1,200 mm
2,500 mm
Advanced for its time
Influenced future designs
|
|
gptkbp:engineConfiguration
|
Limited production
H-24
|
|
gptkbp:enginePower
|
1,800 hp
|
|
gptkbp:engineType
|
Radial engine
Several experimental versions
|
|
gptkbp:firstFlight
|
1943
|
|
gptkbp:firstRace
|
1941
|
|
gptkbp:fuelType
|
Avgas
Direct fuel injection
Dual ignition
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Napier Sabre
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Sea_Fury
gptkb:Hawker_Tempest
de Havilland Mosquito
|
|
gptkbp:manufacturer
|
Napier & Son
|
|
gptkbp:noise_level
|
Loud
|
|
gptkbp:notable_feature
|
Supercharger
|
|
gptkbp:notableUsers
|
gptkb:Royal_Air_Force
gptkb:Royal_Navy
|
|
gptkbp:performance
|
High power-to-weight ratio
|
|
gptkbp:performances
|
Good
High
Moderate
3,000 rpm
|
|
gptkbp:powerOutput
|
2,000 hp
|
|
gptkbp:productionYears
|
1941-1947
|
|
gptkbp:retirementYear
|
1950
|
|
gptkbp:setting
|
Two-row radial engine
|
|
gptkbp:successor
|
gptkb:Napier_Nomad
|
|
gptkbp:torque
|
1,500 lb-ft
|
|
gptkbp:type
|
H-type engine
|
|
gptkbp:weight
|
1,200 lb
|