|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:helicopter
civil helicopters
|
|
gptkbp:combustor_type
|
annular
annular combustion chamber
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:development
|
gptkb:Partnerships
|
|
gptkbp:diameter
|
600 mm
400 mm
|
|
gptkbp:emissions_standard
|
gptkb:EURO_I
|
|
gptkbp:engine
|
gptkb:RTM322-10
gptkb:RTM322-12
gptkb:RTM322-13
gptkb:RTM322-14
gptkb:RTM322-15
gptkb:RTM322-16
gptkb:RTM322-01
gptkb:RTM322-06
Brayton cycle
RTM322-02
RTM322-03
RTM322-11
RTM322-20
RTM322-07
RTM322-09
RTM322-18
RTM322-04
RTM322-05
RTM322-08
RTM322-17
RTM322-19
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:exhaust_system
|
single exhaust
|
|
gptkbp:first_flight
|
gptkb:1990
gptkb:1991
|
|
gptkbp:fuel_economy
|
0.5 kg/s
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Turbomeca RTM322
|
|
gptkbp:introduced
|
gptkb:1990
|
|
gptkbp:launch_window
|
starter-generator
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:power_output
|
1,800 shp
1,500 to 1,800 shp
|
|
gptkbp:propulsion
|
1,800 shp
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:successor
|
gptkb:RTM322-01
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Agusta_Westland_AW159_Wildcat
gptkb:Eurocopter_Tiger
gptkb:NHIndustries_NH90
|
|
gptkbp:video_output
|
axial
|
|
gptkbp:weight
|
150 kg
250 kg
|
|
gptkbp:bfsParent
|
gptkb:Merlin_Mk5
gptkb:Agusta_Westland_AW101
gptkb:Merlin_HM2
gptkb:Merlin_HM1
|
|
gptkbp:bfsLayer
|
6
|