MTU Turbomeca Rolls-Royce MTR390
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:Germany gptkb:United_Kingdom |
| gptkbp:developedBy |
gptkb:Eurocopter_Tiger
|
| gptkbp:diameter |
0.39 m
|
| gptkbp:firstFlight |
1989
|
| https://www.w3.org/2000/01/rdf-schema#label |
MTU Turbomeca Rolls-Royce MTR390
|
| gptkbp:length |
1.3 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:MTU_Aero_Engines gptkb:Turbomeca |
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
1,285 kW
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Eurocopter_Tiger
|
| gptkbp:variant |
gptkb:MTR390-2C
gptkb:MTR390-E |
| gptkbp:weight |
200 kg
|
| gptkbp:bfsParent |
gptkb:Tiger_ARH_helicopter
|
| gptkbp:bfsLayer |
6
|