Sud Aviation SA 318C Alouette II
GPTKB entity
Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:crew |
1
|
| gptkbp:emptyWeight |
950 kg
|
| gptkbp:engineType |
Turbomeca Artouste II turboshaft
|
| gptkbp:firstFlight |
12 March 1955
|
| gptkbp:height |
2.75 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Sud Aviation SA 318C Alouette II
|
| gptkbp:introduced |
1957
|
| gptkbp:length |
9.66 m
|
| gptkbp:mainRotorDiameter |
10.2 m
|
| gptkbp:manufacturer |
gptkb:Sud_Aviation
|
| gptkbp:maximumSpeed |
185 km/h
|
| gptkbp:maxTakeoffWeight |
1,600 kg
|
| gptkbp:notableFor |
first production helicopter powered by a gas turbine engine
|
| gptkbp:primaryUser |
gptkb:French_Army
gptkb:German_Army gptkb:French_Air_Force gptkb:Indian_Air_Force gptkb:French_Navy |
| gptkbp:range |
565 km
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:seatingCapacity |
4
|
| gptkbp:serviceCeiling |
2,200 m
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Aérospatiale_Gazelle
|
| gptkbp:usedIn |
gptkb:military
civilian |
| gptkbp:bfsParent |
gptkb:Royal_Togolese_Air_Force
|
| gptkbp:bfsLayer |
5
|