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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:helicopter
civil helicopters
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gptkbp:certification
|
FAA certified
EASA certified
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gptkbp:combustor_type
|
annular combustion chamber
|
|
gptkbp:compression_ratio
|
16:1
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gptkbp:configuration
|
twin-spool
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gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
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gptkbp:cooling_system
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air-cooled
air cooling
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gptkbp:design
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modular design
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gptkbp:development
|
joint development by Rolls-Royce and Turbomeca
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gptkbp:diameter
|
600 mm
|
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gptkbp:emissions_standard
|
low emissions
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gptkbp:engine
|
gptkb:RTM322-10
gptkb:RTM322-12
gptkb:RTM322-13
gptkb:RTM322-14
gptkb:RTM322-15
gptkb:RTM322-16
RTM322-11
RTM322-20
RTM322-18
RTM322-17
RTM322-19
RTM322-21
RTM322-22
RTM322-23
RTM322-24
RTM322-25
RTM322-9
RTM322-2
RTM322-26
RTM322-27
RTM322-28
RTM322-29
RTM322-3
RTM322-30
RTM322-4
RTM322-5
RTM322-6
RTM322-7
RTM322-8
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gptkbp:first_flight
|
gptkb:1999
|
|
gptkbp:fuel_economy
|
high
|
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gptkbp:fuel_type
|
gptkb:Jet_A-1
|
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gptkbp:gearbox
|
integrated gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RTM322 engine
|
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gptkbp:launch_window
|
starter-generator
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise level
|
|
gptkbp:operational_range
|
-40 to +50 ° C
|
|
gptkbp:power_output
|
1,800 shp
|
|
gptkbp:propulsion
|
1,800 lbf
|
|
gptkbp:successor
|
RTM322-1
|
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gptkbp:type
|
gptkb:turbofan_engine
|
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gptkbp:used_in
|
gptkb:Agusta_Westland_AW159
gptkb:Westland_Lynx
gptkb:Eurocopter_EC725_Caracal
|
|
gptkbp:weight
|
approximately 300 kg
|
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gptkbp:bfsParent
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:bfsLayer
|
5
|