T56 engine

URI: https://gptkb.org/entity/T56_engine
GPTKB entity
Statements (62)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:transport_aircraft
gptkb:military_aircraft
gptkbp:armament gptkb:4
gptkbp:compression_ratio 12:1
gptkbp:configuration twin-shaft
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:development ongoing
gptkbp:diameter 1,200 mm
gptkbp:emissions_standard low
gptkbp:first_flight 1953
gptkbp:fuel_economy good
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label T56 engine
gptkbp:length 1,800 mm
gptkbp:maintenance 3,600 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:noise_level moderate
gptkbp:number_of_stages gptkb:3
gptkbp:operational_range 1,500 nautical miles
gptkbp:power_output 4,600 shp
gptkbp:propeller variable-pitch propeller
gptkbp:propulsion 3.83:1
gptkbp:reliability high
gptkbp:service_ceiling 25,000 feet
gptkbp:successor gptkb:PW150
gptkbp:used_in gptkb:Lockheed_C-130_Hercules
gptkb:Lockheed_P-3_Orion
gptkbp:variant T56-A-1
T56-A-3
T56-A-15
T56-A-427
T56-A-427 A
T56-A-427 B
T56-A-427 C
T56-A-427 D
T56-A-427 E
T56-A-427 F
T56-A-427 G
T56-A-427 H
T56-A-427 I
T56-A-427 J
T56-A-427 K
T56-A-427 L
T56-A-427 M
T56-A-427 N
T56-A-427 O
T56-A-427 P
T56-A-427 Q
T56-A-427 R
T56-A-427 S
T56-A-427 T
T56-A-427 U
T56-A-427 V
T56-A-427 W
T56-A-427 X
T56-A-427 Y
T56-A-427 Z
gptkbp:weight 1,200 kg
gptkbp:bfsParent gptkb:Hercules_engine
gptkbp:bfsLayer 7