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gptkbp:instanceOf
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gptkb:helicopter
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|
gptkbp:armament
|
machine guns
anti-tank missiles
rocket pods
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gptkbp:builtBy
|
gptkb:SOKO_(Yugoslavia)
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gptkbp:capacity
|
3 passengers
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|
gptkbp:crew
|
2
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gptkbp:developedBy
|
gptkb:Aérospatiale_SA.342_Gazelle
gptkb:Sud_Aviation_SA.340
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|
gptkbp:emptyWeight
|
908 kg
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|
gptkbp:enginePower
|
440 kW
|
|
gptkbp:engineType
|
gptkb:Turbomeca_Astazou_IIIA_turboshaft
|
|
gptkbp:exportedTo
|
gptkb:Egypt
gptkb:France
gptkb:Iraq
gptkb:Kuwait
gptkb:Libya
gptkb:Morocco
gptkb:Syria
gptkb:Tunisia
gptkb:United_Kingdom
gptkb:Yugoslavia
gptkb:Zambia
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|
gptkbp:firstFlight
|
7 April 1967
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|
gptkbp:height
|
3.15 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soko SA.341 Gazelle
|
|
gptkbp:introduced
|
1973
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|
gptkbp:length
|
11.97 m
|
|
gptkbp:mainRotorDiameter
|
10.5 m
|
|
gptkbp:manufacturer
|
gptkb:Aérospatiale
gptkb:Sud_Aviation
gptkb:SOKO
|
|
gptkbp:maximumSpeed
|
310 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,800 kg
|
|
gptkbp:notableFeature
|
fenestron tail rotor
|
|
gptkbp:origin
|
gptkb:France
gptkb:Yugoslavia
|
|
gptkbp:primaryUser
|
gptkb:British_Army
gptkb:French_Army
gptkb:Yugoslav_Air_Force
|
|
gptkbp:range
|
670 km
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:serviceCeiling
|
5,000 m
|
|
gptkbp:status
|
in service (as of 2024)
|
|
gptkbp:usedInConflict
|
gptkb:Falklands_War
gptkb:Gulf_War
gptkb:Yugoslav_Wars
|
|
gptkbp:bfsParent
|
gptkb:Yugoslav_Air_Force
|
|
gptkbp:bfsLayer
|
5
|