gptkbp:instanceOf
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gptkb:helicopter
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gptkbp:armament
|
machine guns
|
gptkbp:crew
|
1 pilot
|
gptkbp:design
|
lightweight construction
high maneuverability
versatile mission capabilities
tandem_rotor_configuration
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gptkbp:engineType
|
turboshaft
|
gptkbp:firstFlight
|
1967
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gptkbp:height
|
3.30 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
SA 346 Gazelle
|
gptkbp:length
|
13.20 m
|
gptkbp:manufacturer
|
Sud Aviation
|
gptkbp:maxSpeed
|
130 knots
|
gptkbp:maxTakeoffWeight
|
2,500 kg
|
gptkbp:militaryRank
|
gptkb:Gazelle_343
gptkb:Gazelle_346
gptkb:Gazelle_342
Gazelle 344
Gazelle_345
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gptkbp:notableFeature
|
gptkb:Gazelle_SA_341
gptkb:Gazelle_SA_343
gptkb:Gazelle_SA_342
|
gptkbp:operationalHistory
|
used in various conflicts
used for training purposes
used for medical evacuation
used for reconnaissance missions
used for search and rescue missions
used for transport missions
|
gptkbp:passengerCapacity
|
5
|
gptkbp:powerOutput
|
650 shp
|
gptkbp:primaryUser
|
gptkb:Brazil
gptkb:France
gptkb:Jordan
gptkb:South_Africa
gptkb:United_Kingdom
|
gptkbp:productionYears
|
1967-1997
|
gptkbp:range
|
600 km
|
gptkbp:role
|
utility helicopter
|
gptkbp:rotorDiameter
|
11.00 m
|
gptkbp:safetyFeatures
|
crashworthy design
dual controls
emergency flotation system
automatic flight control system
|
gptkbp:services
|
4,500 m
|
gptkbp:totalGoals
|
over 1,000
|
gptkbp:usedBy
|
military forces
|
gptkbp:weight
|
1,200 kg
|