|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:aircraft
|
rotorcraft
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:crewCapacity
|
2
|
|
gptkbp:design
|
military transport
twin-engine
Boeing_engineers
|
|
gptkbp:developer
|
Boeing_Vertol_360_program
|
|
gptkbp:electrification
|
2 × Lycoming T53
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:firstFlight
|
1980
|
|
gptkbp:fuelCapacity
|
1,200 liters
|
|
gptkbp:height
|
3.5 meters
|
|
gptkbp:historicalSignificance
|
early tandem rotor design.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing Vertol 360-2
|
|
gptkbp:influences
|
Boeing_360_series
|
|
gptkbp:introduced
|
1980
|
|
gptkbp:landingGear
|
retractable
|
|
gptkbp:legacy
|
influenced future helicopters
|
|
gptkbp:length
|
12.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Boeing_Vertol
|
|
gptkbp:market
|
military and civilian
|
|
gptkbp:maxSpeed
|
150 knots
|
|
gptkbp:maxTakeoffWeight
|
4,500 kg
|
|
gptkbp:navigationEquipment
|
advanced avionics
|
|
gptkbp:notableFeature
|
dual rotor system
|
|
gptkbp:operationalRange
|
250 nautical miles
|
|
gptkbp:passengerCapacity
|
12
|
|
gptkbp:primaryUser
|
gptkb:U.S._military
|
|
gptkbp:produces
|
limited series
|
|
gptkbp:productionLocation
|
gptkb:Pennsylvania
|
|
gptkbp:productionYears
|
1980-1990
|
|
gptkbp:range
|
300 nautical miles
|
|
gptkbp:relatedAircraft
|
gptkb:Boeing_CH-47_Chinook
Boeing_CH-46_Sea_Knight
|
|
gptkbp:retirementYear
|
1995
|
|
gptkbp:role
|
transport
utility helicopter
|
|
gptkbp:rotorDiameter
|
10.7 meters
|
|
gptkbp:safetyFeatures
|
crashworthy design
|
|
gptkbp:secondaryRole
|
transport and logistics
|
|
gptkbp:services
|
1981
15,000 feet
|
|
gptkbp:setting
|
gptkb:tandem_rotor
multi-role
|
|
gptkbp:status
|
retired
|
|
gptkbp:variant
|
Boeing_Vertol_360-2A
Boeing_Vertol_360-2B
|
|
gptkbp:weight
|
3,600 kg
|