|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:builtBy
|
gptkb:Hindustan_Aeronautics_Limited
|
|
gptkbp:category
|
gptkb:helicopter
civil utility helicopter
|
|
gptkbp:crew
|
1
|
|
gptkbp:derivedFrom
|
gptkb:Aérospatiale_Alouette_II
gptkb:Aérospatiale_Alouette_III
|
|
gptkbp:emptyWeight
|
1,021 kg
|
|
gptkbp:enginePower
|
858 shp
|
|
gptkbp:engineType
|
gptkb:Turbomeca_Artouste_IIIB_turboshaft
|
|
gptkbp:firstFlight
|
1969
|
|
gptkbp:height
|
3.09 m
|
|
gptkbp:introduced
|
1971
|
|
gptkbp:length
|
10.24 m
|
|
gptkbp:licenseBuiltAs
|
gptkb:HAL_Cheetah
|
|
gptkbp:mainRotorDiameter
|
11.02 m
|
|
gptkbp:manufacturer
|
gptkb:Aérospatiale
|
|
gptkbp:maximumSpeed
|
192 km/h
|
|
gptkbp:maxTakeoffWeight
|
2,300 kg
|
|
gptkbp:notableFor
|
high-altitude performance
|
|
gptkbp:origin
|
gptkb:France
|
|
gptkbp:primaryUser
|
gptkb:French_Army
gptkb:Indian_Air_Force
|
|
gptkbp:range
|
515 km
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:seatingCapacity
|
4
|
|
gptkbp:serviceCeiling
|
7,000 m
|
|
gptkbp:status
|
retired (France)
active (India)
|
|
gptkbp:bfsParent
|
gptkb:RAF_Andover
gptkb:Turbine_G3_engine
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Aérospatiale Lama
|