Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbine engine
|
| gptkbp:application |
gptkb:Eurocopter_AS350
gptkb:Bell_407 gptkb:Eurocopter_EC120 Agusta A109 |
| gptkbp:diameter |
0.4 m
|
| gptkbp:engineConfiguration |
free turbine
|
| gptkbp:engineType |
axial compressor
single-stage turbine |
| gptkbp:firstFlight |
1970
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Arriel 1B
|
| gptkbp:length |
1.1 m
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:powerOutput |
500 shp
|
| gptkbp:type |
turbo-shaft engine
|
| gptkbp:usedIn |
helicopters
|
| gptkbp:weight |
120 kg
|