Statements (56)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
helicopter engine
|
| gptkbp:application |
military helicopters
civil helicopters |
| gptkbp:certifications |
EASA_certified
|
| gptkbp:climate |
up to 900 °C
|
| gptkbp:compressionRatio |
16:1
|
| gptkbp:controls |
starter-generator
FADEC |
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design |
modular design
|
| gptkbp:diameter |
0.5 m
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissionsStandard |
EURO I
|
| gptkbp:engine |
gptkb:RTM322
0.5 m 1.5 m 150 kg 0.6 m military and civilian use |
| gptkbp:engineConfiguration |
gptkb:Rolls-Royce
V-type engine |
| gptkbp:enginePower |
800 shp
|
| gptkbp:engineType |
high performance
lightweight construction advanced materials modular architecture high reliability low maintenance environmentally friendly compact design high efficiency free turbine digital control system two-stage turbine turboshaft engine three-stage compressor |
| gptkbp:firstRace |
1998
|
| gptkbp:fuel_capacity |
200 l/h
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular combustion chamber |
| https://www.w3.org/2000/01/rdf-schema#label |
RTM322-08
|
| gptkbp:is_used_in |
gptkb:Eurocopter_EC635
AgustaWestland AW159 Wildcat |
| gptkbp:length |
1.5 m
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:maximum_speed |
42,000 RPM
|
| gptkbp:noise_level |
85 dB
|
| gptkbp:powerOutput |
800 shp
|
| gptkbp:propulsion |
5.3 shp/kg
|
| gptkbp:related_engine |
RTM series
|
| gptkbp:service_ceiling |
6000 m
|
| gptkbp:setting |
Vee_configuration
|
| gptkbp:torque |
1000 Nm
|
| gptkbp:type |
turbo-shaft engine
|
| gptkbp:weight |
150 kg
|