|
gptkbp:instanceOf
|
turboshaft engine
|
|
gptkbp:application
|
military helicopters
|
|
gptkbp:certifications
|
EASA_certified
|
|
gptkbp:climate
|
up to 1,000 °C
|
|
gptkbp:collaborations
|
Turbomeca_and_Rolls-Royce
|
|
gptkbp:compressionRatio
|
16:1
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:developer
|
joint_venture_with_Turbomeca
|
|
gptkbp:diameter
|
600 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
EURO I
|
|
gptkbp:engine
|
horizontal layout
|
|
gptkbp:engineType
|
free turbine
starter-generator
turbo-shaft
up to 1,200 °C
RTM322-01, RTM322-02, RTM322-03
|
|
gptkbp:firstFlight
|
1997
|
|
gptkbp:fuel_capacity
|
200 l/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
dual fuel system
can-annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RTM322
|
|
gptkbp:introduced
|
1990s
|
|
gptkbp:is_monitored_by
|
digital monitoring system
|
|
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:Rolls-Royce_Holdings
|
|
gptkbp:market_segment
|
military aviation
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:operational_status
|
gptkb:NATO_forces
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:performances
|
up to 5,000 hours
major overhaul every 2,500 hours
|
|
gptkbp:powerOutput
|
1,800 shp
|
|
gptkbp:propulsion
|
6 hp/kg
1,800 lbf
|
|
gptkbp:related_engine
|
Turbomeca Makila
RTM322_family
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:setting
|
Vee_engine
|
|
gptkbp:weight
|
300 kg
|