Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
2
|
| gptkbp:emptyWeight |
410 kg
|
| gptkbp:engine |
Turbomeca Palouste
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1953
|
| gptkbp:height |
2.35 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Sud-Ouest Djinn
|
| gptkbp:introduced |
1954
|
| gptkbp:length |
6.6 m
|
| gptkbp:manufacturer |
gptkb:Sud-Ouest
|
| gptkbp:maximumSpeed |
150 km/h
|
| gptkbp:maxTakeoffWeight |
700 kg
|
| gptkbp:notableFor |
first production helicopter powered by a gas turbine
|
| gptkbp:numberBuilt |
178
|
| gptkbp:primaryUser |
gptkb:French_Army
|
| gptkbp:range |
220 km
|
| gptkbp:role |
gptkb:helicopter
training helicopter |
| gptkbp:rotorConfiguration |
coaxial
|
| gptkbp:serviceCeiling |
2,500 m
|
| gptkbp:status |
retired
|
| gptkbp:type |
gptkb:helicopter
|
| gptkbp:usedBy |
gptkb:French_Army
gptkb:German_Army gptkb:Indian_Air_Force gptkb:Austrian_Air_Force gptkb:Swiss_Air_Force |
| gptkbp:bfsParent |
gptkb:Turbomeca_Aubisque
gptkb:Turbomeca_Artouste_II |
| gptkbp:bfsLayer |
7
|