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gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:configuration
|
gptkb:helicopter
|
|
gptkbp:country_of_origin
|
gptkb:France
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
single rotor
|
|
gptkbp:diameter
|
11.0 m
fenestron
|
|
gptkbp:engine
|
gptkb:Turbomeca_Artouste_IIA
|
|
gptkbp:engine_type
|
turboshaft
|
|
gptkbp:first_flight
|
gptkb:1955
1990s
|
|
gptkbp:fuel_capacity
|
300 L
|
|
gptkbp:fuselage_material
|
metal construction
|
|
gptkbp:height
|
3.2 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Aérospatiale Alouette II
|
|
gptkbp:introduced
|
gptkb:1956
|
|
gptkbp:landing_gear
|
skids
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Aérospatiale
|
|
gptkbp:max_speed
|
210 km/h
|
|
gptkbp:max_takeoff_weight
|
2,200 kg
|
|
gptkbp:military_technology
|
gptkb:transportation
gptkb:emergency_services
gptkb:training
aerial photography
reconnaissance
|
|
gptkbp:notable_users
|
gptkb:French_Army
gptkb:Indian_Air_Force
gptkb:South_African_Air_Force
gptkb:Swiss_Air_Force
gptkb:Belgian_Air_Force
|
|
gptkbp:number_built
|
1,500
|
|
gptkbp:passenger_capacity
|
gptkb:3
|
|
gptkbp:powers
|
560 hp
|
|
gptkbp:produces
|
1955-1985
|
|
gptkbp:propulsion
|
single engine
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retired
|
gptkb:1985
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:service_entry
|
gptkb:1956
|
|
gptkbp:successor
|
gptkb:Aérospatiale_Gazelle
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:used_by
|
gptkb:military
civilian
|
|
gptkbp:variant
|
Alouette III
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:wingspan
|
11.0 m
|
|
gptkbp:bfsParent
|
gptkb:Turbomeca_Turmo
|
|
gptkbp:bfsLayer
|
7
|