|
gptkbp:instanceOf
|
engine
|
|
gptkbp:application
|
Military and civilian aircraft
|
|
gptkbp:compressionRatio
|
6.5:1
|
|
gptkbp:controls
|
Automatic control system
|
|
gptkbp:coolingSystem
|
Air-cooled
|
|
gptkbp:cylinderCount
|
18
Double Wasp
|
|
gptkbp:displacement
|
3350 cubic inches
|
|
gptkbp:engine
|
Electric starter
Detailed specifications available.
Fuselage-mounted
Exhaust stacks
Oil cooling system
Single-stage turbocharger
|
|
gptkbp:engineConfiguration
|
Radial
|
|
gptkbp:engineDisplacement
|
Modular_design
|
|
gptkbp:engineType
|
gptkb:Piston_engine
High reliability
R-3350-23, R-3350-32
|
|
gptkbp:firstFlight
|
1946
|
|
gptkbp:fuelType
|
Avgas
Dual ignition
Pressure carburetor
|
|
gptkbp:hasArea
|
Extensive testing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-3350-66
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:notableUsers
|
gptkb:Lockheed_Constellation
|
|
gptkbp:operationalHistory
|
Developed post-WWII
|
|
gptkbp:operationalRange
|
High altitude
|
|
gptkbp:performances
|
1,500 hours
|
|
gptkbp:powerOutput
|
2000 horsepower
|
|
gptkbp:productionYears
|
1946-1955
|
|
gptkbp:propulsion
|
Variable-pitch propeller
|
|
gptkbp:relatedPatent
|
R-2800
|
|
gptkbp:successor
|
R-3350-26W
|
|
gptkbp:type
|
gptkb:Radial_Engine
|
|
gptkbp:usedIn
|
gptkb:Douglas_DC-7
|
|
gptkbp:weight
|
approximately 1,500 pounds
|