Statements (23)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:jet_engine
|
gptkbp:application |
helicopters
|
gptkbp:combustor_type |
annular combustor
|
gptkbp:compressor_type |
gptkb:3
|
gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
gptkbp:design |
high bypass ratio
|
gptkbp:diameter |
1.2 m
|
gptkbp:emissions_standard |
low emissions
|
gptkbp:first_introduced |
gptkb:2010
|
gptkbp:fuel_economy |
0.5 kg/k N/h
|
gptkbp:fuel_type |
gptkb:Jet_A-1
|
https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce K60
|
gptkbp:maintenance |
500 hours
|
gptkbp:manufacturer |
gptkb:Ford_Motor_Company
|
gptkbp:noise_level |
low noise
|
gptkbp:propulsion |
60 k N
|
gptkbp:turbine_type |
2
|
gptkbp:type |
gptkb:turbofan_engine
|
gptkbp:used_in |
gptkb:military_aircraft
|
gptkbp:weight |
approximately 200 kg
|
gptkbp:bfsParent |
gptkb:Rolls-Royce_Meteor_V12
gptkb:Rolls-Royce_Meteor |
gptkbp:bfsLayer |
4
|