|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
none
|
|
gptkbp:availability
|
available for lease
|
|
gptkbp:avionics
|
modern avionics
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:crewCapacity
|
2
|
|
gptkbp:design
|
Boeing_Vertol_Company
twin_rotor_design
|
|
gptkbp:enginePower
|
2,500 shp
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:environment
|
operates in various environments
|
|
gptkbp:firstFlight
|
1980
|
|
gptkbp:fuelCapacity
|
1,500 liters
|
|
gptkbp:height
|
5.1 m
|
|
gptkbp:historicalSignificance
|
significant in helicopter development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing Vertol 234-1
|
|
gptkbp:influences
|
influenced_by_earlier_Vertol_designs
|
|
gptkbp:introduced
|
1980
|
|
gptkbp:landingGear
|
retractable
|
|
gptkbp:legacy
|
remains in use today
|
|
gptkbp:length
|
19.5 m
|
|
gptkbp:maintenance
|
requires regular maintenance
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:market
|
commercial and military
|
|
gptkbp:maxSpeed
|
150 knots
|
|
gptkbp:maxTakeoffWeight
|
6,800 kg
7,500 kg
|
|
gptkbp:modifications
|
various configurations available
|
|
gptkbp:notableFeature
|
twin_rotor_system
|
|
gptkbp:numberBuilt
|
100
|
|
gptkbp:operationalArea
|
used for troop transport
|
|
gptkbp:operationalHistory
|
used in various military operations
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:passengerCapacity
|
30
3,000 kg
|
|
gptkbp:performance
|
high payload capacity
|
|
gptkbp:primaryUser
|
military
|
|
gptkbp:produces
|
1979-1985
|
|
gptkbp:propulsion
|
2 engines
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:relatedAircraft
|
gptkb:Boeing_CH-47_Chinook
|
|
gptkbp:role
|
transport
|
|
gptkbp:rotorDiameter
|
18.3 m
|
|
gptkbp:safetyFeatures
|
crashworthy design
|
|
gptkbp:services
|
4,600 m
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Boeing_CH-47F_Chinook
|
|
gptkbp:training
|
used for pilot training
|
|
gptkbp:type
|
utility helicopter
|
|
gptkbp:variant
|
gptkb:Boeing_Vertol_234
|
|
gptkbp:wingspan
|
not applicable
|