Rolls-Royce Turbomeca RTM322
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
military helicopters
civil helicopters |
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_Kingdom |
| gptkbp:diameter |
0.5 m
|
| gptkbp:firstRun |
1990
|
| gptkbp:fuelType |
gptkb:gasoline
|
| gptkbp:length |
1.1 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Turbomeca |
| gptkbp:numberOfStages |
2 axial, 1 centrifugal
2 high-pressure, 2 power turbine |
| gptkbp:powerOutput |
2100 to 2700 shp
|
| gptkbp:successor |
gptkb:Safran_Aneto
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:NHIndustries_NH90
gptkb:AgustaWestland_AW101 gptkb:Apache_AH1 |
| gptkbp:weight |
approximately 350 kg
|
| gptkbp:bfsParent |
gptkb:AgustaWestland_Apache
gptkb:MRH-90_Taipan_helicopter |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Turbomeca RTM322
|