R-3350-26

GPTKB entity

Statements (50)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:aircraft_operated gptkb:B-29_Superfortress
gptkb:Convair_340
gptkb:Convair_440
gptkb:Lockheed_L-049_Constellation
gptkb:Douglas_C-54_Skymaster
gptkb:Lockheed_L-1049_Super_Constellation
gptkb:Lockheed_L-749_Constellation
gptkb:Boeing_377_Stratocruiser
gptkb:Douglas_C-118_Liftmaster
gptkb:Douglas_DC-6
gptkb:Boeing_Stratocruiser
gptkb:Martin_PBM_Mariner
Boeing 707 (early models)
gptkbp:compression_ratio 7.0:1
gptkbp:configuration 14-cylinder
gptkbp:cooling_system air-cooled
gptkbp:displacement 3350 cubic inches
gptkbp:engine gptkb:Pratt_&_Whitney_R-2800
gptkb:Pratt_&_Whitney_R-4360
yes
four-stroke
gptkbp:engine_configuration radial
horizontally opposed
gptkbp:first_flight 1941
gptkbp:fuel_economy 0.5 pounds per horsepower per hour
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label R-3350-26
gptkbp:ignition_system dual ignition
gptkbp:maintenance 100 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:operational_history used in World War II
used in Korean War
gptkbp:original_run 1941
gptkbp:power_output 2000 horsepower
gptkbp:produces over 30,000
gptkbp:production_years gptkb:1955
gptkbp:propulsion 1.11
gptkbp:replaced_by turboprop engines
gptkbp:type gptkb:radial_engine
gptkbp:used_in gptkb:Boeing_B-17_Flying_Fortress
gptkb:Lockheed_Constellation
gptkb:Douglas_DC-7
gptkbp:valve_configuration pushrod
gptkbp:variant gptkb:R-3350-32
R-3350-54
R-3350-23
gptkbp:weight approximately 1,800 pounds
gptkbp:bfsParent gptkb:Wright_R-3350
gptkbp:bfsLayer 5