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gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Airco_DH.9
gptkb:De_Havilland_DH.9
|
|
gptkbp:aircraft_operated
|
gptkb:Bell_212
gptkb:Boeing_CH-47_Chinook
gptkb:Westland_Wessex
gptkb:Sikorsky_S-61
gptkb:Mil_Mi-8
Agusta Westland A W101
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
gptkb:2001
|
|
gptkbp:design
|
gptkb:Siddeley_Aircraft
Siddeley Aircraft engineers
|
|
gptkbp:diameter
|
14.63 m
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Gnome
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Siddeley Puma
|
|
gptkbp:introduced
|
gptkb:1965
|
|
gptkbp:is_used_by
|
gptkb:military_unit
gptkb:military_base
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Siddeley_Aircraft
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
4,500 kg
|
|
gptkbp:notable_features
|
high payload capacity
versatile mission capabilities
reliable in adverse weather conditions
good performance in hot climates
twin rotor system
|
|
gptkbp:number_built
|
over 700
|
|
gptkbp:operational_range
|
600 km
|
|
gptkbp:origin
|
gptkb:United_Kingdom
|
|
gptkbp:primary_user
|
gptkb:British_Armed_Forces
|
|
gptkbp:produced_by
|
1965-1985
|
|
gptkbp:propulsion
|
twin-engine
|
|
gptkbp:range
|
800 km
|
|
gptkbp:role
|
gptkb:helicopter
transport helicopter
|
|
gptkbp:seating_capacity
|
gptkb:12
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:services
|
gptkb:1966
gptkb:2015
|
|
gptkbp:successor
|
Eurocopter A S332 Super Puma
Westland Puma H C1
|
|
gptkbp:type
|
multi-role helicopter
|
|
gptkbp:variant
|
gptkb:Puma_Mk_1
gptkb:Puma_Mk_2
Puma H C1
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingspan
|
14.63 m
|