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gptkbp:instanceOf
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gptkb:helicopter
|
|
gptkbp:aircraft
|
civil and military aircraft
|
|
gptkbp:armament
|
none
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gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:cockpit
|
two-seat cockpit
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|
gptkbp:crew
|
2
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gptkbp:currentStatus
|
no longer in production
|
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gptkbp:design
|
high-set main rotor
modular design approach
|
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gptkbp:developer
|
Westland 50 series
|
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gptkbp:engineConfiguration
|
gptkb:Rolls-Royce
|
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gptkbp:enginePower
|
1,000 shp
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:fuelCapacity
|
1,200 liters
|
|
gptkbp:headlights
|
1
|
|
gptkbp:historicalSignificance
|
part_of_British_helicopter_development_history
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Westland 50 Mk 2
|
|
gptkbp:influences
|
previous_Westland_designs
|
|
gptkbp:landingGear
|
skid type
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
Westland_Aircraft
|
|
gptkbp:market
|
commercial and military
|
|
gptkbp:marketSegment
|
light utility helicopters
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
4,500 kg
|
|
gptkbp:notableFeature
|
2
none reported
versatile and adaptable design
|
|
gptkbp:operationalHistory
|
used in various roles
|
|
gptkbp:operationalRange
|
effective operational range of 600 km
|
|
gptkbp:passengerCapacity
|
6
1,000 kg
|
|
gptkbp:performance
|
good performance in various conditions
|
|
gptkbp:primaryUser
|
military
|
|
gptkbp:productionLocation
|
gptkb:Yeovil,_England
|
|
gptkbp:productionYears
|
1970-1980
|
|
gptkbp:range
|
600 km
|
|
gptkbp:relatedModel
|
gptkb:Westland_50_Mk_1
|
|
gptkbp:retirementYear
|
1980s
|
|
gptkbp:role
|
utility helicopter
|
|
gptkbp:rotorDiameter
|
11.0 m
|
|
gptkbp:safetyFeatures
|
generally good safety record
|
|
gptkbp:services
|
3,000 m
|
|
gptkbp:setting
|
twin-engine configuration
|
|
gptkbp:successor
|
gptkb:Westland_30
|
|
gptkbp:team
|
Westland_design_team
|
|
gptkbp:totalGoals
|
approximately 100 units
|
|
gptkbp:variant
|
gptkb:Westland_50_Mk_1
|
|
gptkbp:weight
|
2,500 kg
|