R-3350-60

GPTKB entity

Properties (61)
Predicate Object
gptkbp:instanceOf engine
gptkbp:compressionRatio 6.5:1
gptkbp:controls Throttle-controlled
gptkbp:coolingSystem Air-cooled
gptkbp:cylinderCount 18
Double Wasp
gptkbp:displacement 3350 cubic inches
gptkbp:drivetrain Pushrod
gptkbp:engine No
Yes
Electric starter
approximately 6.5 feet
Effective cooling system.
Air-cooled with external fins.
Commercial and military aviation.
Detailed in various aviation manuals.
Fuel cut-off.
Incorporated advanced technologies for its time.
Known for its power and performance.
Maintenance and reliability issues.
Nacelle-mounted
Phased out in the 1960s.
Significant impact on aviation technology.
Used high-octane aviation fuel.
gptkbp:engineConfiguration Radial
Complex radial design.
gptkbp:engineDisplacement Designed for long-range bombers.
approximately 4.5 feet
gptkbp:engineType Reciprocating Engine
High power-to-weight ratio.
Multiple variants with different specifications.
Widely used in the 1950s.
gptkbp:firstFlight 1946
gptkbp:firstHeld gptkb:Lockheed_L-1049_Super_Constellation
gptkb:Boeing_377_Stratocruiser
gptkbp:fuelCapacity 0.5 to 0.6 pounds per horsepower per hour
gptkbp:fuelType Avgas
Dual ignition
gptkbp:hasArea Tested on dynamometers.
https://www.w3.org/2000/01/rdf-schema#label R-3350-60
gptkbp:maintenance 100 hours
gptkbp:manufacturer gptkb:Wright_Aeronautical_Corporation
gptkbp:notableFeature gptkb:R-3350-26
R-3350-32
R-3350-54
R-3350-23
gptkbp:operationalHistory Used in military and civilian aircraft.
Developed_during_World_War_II.
gptkbp:operationalStatus up to 25,000 feet
gptkbp:performances 2000 hours
Influenced later radial engine designs.
gptkbp:powerOutput 2000 to 3500 horsepower
gptkbp:productionYears 1940s to 1950s
gptkbp:propulsion up to 3500 pounds
gptkbp:setting Air-cooled
gptkbp:successor R-4360
gptkbp:type gptkb:Radial_Engine
gptkbp:usedIn gptkb:Lockheed_Constellation
gptkb:Boeing_377_Stratocruiser
gptkb:Douglas_DC-7
gptkbp:weight approximately 1,800 pounds