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gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:crew
|
1
|
|
gptkbp:developedBy
|
gptkb:SNCASE_SE.3120_Alouette
|
|
gptkbp:displayedAt
|
gptkb:South_African_Air_Force_Museum
gptkb:Deutsches_Museum
gptkb:Musée_de_l’Air_et_de_l’Espace
|
|
gptkbp:emptyWeight
|
950 kg
|
|
gptkbp:engine
|
gptkb:Turbomeca_Artouste_II
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:exportedTo
|
over 40 countries
|
|
gptkbp:firstFlight
|
1955-03-12
|
|
gptkbp:height
|
2.75 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Alouette II
|
|
gptkbp:introduced
|
1956
|
|
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:numberBuilt
|
over 1300
|
|
gptkbp:primaryUser
|
gptkb:South_African_Air_Force
gptkb:French_Army
gptkb:German_Army
gptkb:Indian_Air_Force
|
|
gptkbp:range
|
565 km
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:seatingCapacity
|
4
|
|
gptkbp:serviceCeiling
|
2,500 m
|
|
gptkbp:successor
|
gptkb:Aérospatiale_Gazelle
|
|
gptkbp:usedIn
|
gptkb:military_operation
training
search and rescue
civilian transport
aerial observation
|
|
gptkbp:bfsParent
|
gptkb:Maltese_Air_Force
gptkb:Alouette_III
gptkb:Force_Aérienne_de_Haute-Volta
|
|
gptkbp:bfsLayer
|
6
|