|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
military transport aircraft
transport aircraft
maritime patrol aircraft
firefighting aircraft
aerial refueling aircraft
search and rescue aircraft
special mission aircraft
cargo_aircraft
|
|
gptkbp:compressionRatio
|
axial compressor
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
intercooling
|
|
gptkbp:design
|
high performance
|
|
gptkbp:developer
|
developed_from_Rolls-Royce_Dart
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:engineType
|
4
free turbine
|
|
gptkbp:firstFlight
|
1954
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce T56
|
|
gptkbp:is_used_in
|
gptkb:Lockheed_C-130_Hercules
gptkb:Lockheed_P-3_Orion
|
|
gptkbp:landing_gear
|
planetary gear
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
long
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_feature
|
T56-A-1
T56-A-3
T56-A-15
T56-A-427
|
|
gptkbp:operationalRange
|
long
|
|
gptkbp:powerOutput
|
1,600 to 4,600 shp
|
|
gptkbp:produces
|
over 20,000
|
|
gptkbp:propulsion
|
0.5
variable-pitch propeller
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:serviceHistory
|
used in military aircraft
used in civilian aircraft
|
|
gptkbp:setting
|
twin-shaft
|
|
gptkbp:weight
|
1,200 kg
|