gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:aircraft
|
utility helicopter
|
gptkbp:airlines
|
2 pilots
|
gptkbp:armament
|
machine guns
|
gptkbp:constructionMaterial
|
aluminum alloy
|
gptkbp:crewCapacity
|
2
|
gptkbp:currentStatus
|
retired from service
|
gptkbp:design
|
Boeing_Vertol_engineers
twin_rotor
|
gptkbp:enginePower
|
2,500 shp
|
gptkbp:engineType
|
turboshaft
|
gptkbp:exhibits
|
in aviation museums
|
gptkbp:firstFlight
|
1980
|
gptkbp:fuelCapacity
|
1,500 L
|
gptkbp:headlights
|
not applicable
|
gptkbp:height
|
4.5 m
|
gptkbp:historicalSignificance
|
important in helicopter development
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing Vertol 234
|
gptkbp:influences
|
design of future helicopters
|
gptkbp:length
|
19.5 m
|
gptkbp:manufacturer
|
gptkb:Boeing_Vertol
|
gptkbp:market
|
military and civilian
|
gptkbp:maximumDepth
|
5,000 kg
|
gptkbp:maxSpeed
|
260 km/h
|
gptkbp:maxTakeoffWeight
|
10,000 kg
|
gptkbp:modifications
|
various military configurations
|
gptkbp:notableFeature
|
dual rotor system
|
gptkbp:numberOfEpisodes
|
2
|
gptkbp:operationalRange
|
1,200 km
|
gptkbp:operationalStatus
|
high
various global regions
|
gptkbp:passengerCapacity
|
30
4,500 kg
side door
|
gptkbp:primaryUser
|
military
|
gptkbp:productionCompany
|
1980-1997
over 200 units
|
gptkbp:propulsion
|
twin-engine
|
gptkbp:range
|
1,000 km
|
gptkbp:relatedModel
|
gptkb:Boeing_Vertol_107
|
gptkbp:retirementYear
|
1997
|
gptkbp:role
|
transport helicopter
|
gptkbp:safetyFeatures
|
generally safe
|
gptkbp:service_ceiling
|
4,600 m
|
gptkbp:serviceHistory
|
used in various military operations
|
gptkbp:services
|
1983
|
gptkbp:successor
|
gptkb:Boeing_CH-47_Chinook
|
gptkbp:takeoffDistance
|
1,200 m
1,000 m
|
gptkbp:variant
|
gptkb:Boeing_Vertol_234LR
|
gptkbp:wingspan
|
15.2 m
|