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gptkbp:instanceOf
|
turboshaft engine
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|
gptkbp:application
|
military helicopters
civil helicopters
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|
gptkbp:certifications
|
gptkb:EASA
gptkb:FAA
|
|
gptkbp:climate
|
up to 1,000 °C
|
|
gptkbp:competitors
|
gptkb:Honeywell_T53
gptkb:Pratt_&_Whitney_Canada_PT6
gptkb:General_Electric_T700
|
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gptkbp:compressionRatio
|
16:1
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|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
modular design
|
|
gptkbp:developer
|
joint development
|
|
gptkbp:diameter
|
400 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
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gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
free turbine
|
|
gptkbp:firstFlight
|
1990
|
|
gptkbp:fuel_capacity
|
0.5 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Turbomeca RTM322
|
|
gptkbp:is_used_in
|
gptkb:Eurocopter_Tiger
AgustaWestland AW159 Wildcat
NHIndustries NH90
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
gptkb:Rolls-Royce
|
|
gptkbp:market
|
global market
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:powerOutput
|
1,500 to 1,800 shp
|
|
gptkbp:propulsion
|
1,800 shp
|
|
gptkbp:related_engine
|
gptkb:RTM322-05
RTM322-01
RTM322-02
RTM322-03
RTM322-04
|
|
gptkbp:serviceType
|
1997
|
|
gptkbp:successor
|
gptkb:RTM322-08
RTM322-06
RTM322-07
RTM322-09
RTM322-10
|
|
gptkbp:type
|
turboshaft engine
|
|
gptkbp:weight
|
250 kg
|