gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:armament
|
none
|
gptkbp:avionics
|
modern navigation systems
|
gptkbp:cockpit
|
1
|
gptkbp:constructionMaterial
|
aluminum alloy
|
gptkbp:crew
|
2
|
gptkbp:currentStatus
|
retired from service
|
gptkbp:design
|
gptkb:Westland_Aircraft_Company
multi-role operations
|
gptkbp:engineType
|
turboshaft
|
gptkbp:firstFlight
|
1971
|
gptkbp:fuelCapacity
|
1,200 L
|
gptkbp:height
|
4.57 m
|
gptkbp:historicalSignificance
|
first British helicopter with a fully composite rotor blade
|
https://www.w3.org/2000/01/rdf-schema#label
|
Westland 1200 Mk 1
|
gptkbp:landingGear
|
skid
|
gptkbp:length
|
15.24 m
|
gptkbp:manufacturer
|
Westland_Aircraft
|
gptkbp:maxSpeed
|
250 km/h
|
gptkbp:maxTakeoffWeight
|
4,500 kg
|
gptkbp:notableFeature
|
1972
high payload capacity
|
gptkbp:numberOfEpisodes
|
2
|
gptkbp:operationalArea
|
civil and military
|
gptkbp:operationalRange
|
600 km
|
gptkbp:participatesIn
|
transport and logistics
|
gptkbp:passengerCapacity
|
12
1,500 kg
|
gptkbp:performance
|
high maneuverability
|
gptkbp:primaryUser
|
gptkb:United_Kingdom
|
gptkbp:productionCompany
|
1980
|
gptkbp:productionStartYear
|
1971
|
gptkbp:propulsion
|
turboshaft engines
|
gptkbp:range
|
800 km
|
gptkbp:relatedAircraft
|
gptkb:Westland_Lynx
|
gptkbp:retirementYear
|
1990
|
gptkbp:role
|
utility helicopter
|
gptkbp:rotorDiameter
|
14.00 m
|
gptkbp:safetyFeatures
|
crashworthy design
|
gptkbp:serviceHistory
|
used in various military operations
|
gptkbp:services
|
4,500 m
|
gptkbp:setting
|
twin-engine
|
gptkbp:successor
|
gptkb:Westland_2000
|
gptkbp:totalGoals
|
100
|
gptkbp:usedBy
|
gptkb:British_Army
gptkb:Royal_Air_Force
|
gptkbp:variant
|
gptkb:Westland_1200_Mk_2
|
gptkbp:weight
|
2,500 kg
|
gptkbp:wingspan
|
14.63 m
|