Boeing Vertol 234

GPTKB entity

Properties (51)
Predicate Object
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