gptkbp:instanceOf
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gptkb:helicopter
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gptkbp:aircraft
|
rotorcraft
transport and utility
|
gptkbp:airlines
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1 pilot
|
gptkbp:avionics
|
basic flight instruments
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gptkbp:category
|
light helicopter
|
gptkbp:crew
|
1 pilot
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gptkbp:design
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gptkb:Stanley_Hiller_Jr.
coaxial_rotor_system
coaxial_rotor_technology
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gptkbp:engine
|
Lycoming VO-540
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gptkbp:firstFlight
|
1953
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gptkbp:fuelCapacity
|
40 gallons
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gptkbp:hasCompetitors
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gptkb:Bell_47
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gptkbp:height
|
9 feet 6 inches
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gptkbp:historicalSignificance
|
early coaxial helicopter design
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hiller 360B
|
gptkbp:landingGear
|
skids
|
gptkbp:legacy
|
influenced future helicopter designs
|
gptkbp:length
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30 feet 6 inches
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gptkbp:manufacturer
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gptkb:Hiller_Aircraft_Corporation
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gptkbp:market
|
civil aviation market
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gptkbp:maxSpeed
|
120 knots
|
gptkbp:maxTakeoffWeight
|
3,200 lbs
|
gptkbp:notableUsers
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gptkb:United_States_Army
|
gptkbp:numberBuilt
|
approximately 200
|
gptkbp:operationalHistory
|
used in various civilian roles
|
gptkbp:passengerCapacity
|
up to 3 passengers
|
gptkbp:performance
|
good maneuverability
|
gptkbp:produces
|
limited series production
|
gptkbp:productionYears
|
1953-1965
|
gptkbp:propulsion
|
turbine engine
|
gptkbp:range
|
300 miles
|
gptkbp:relatedModel
|
gptkb:Hiller_12E
|
gptkbp:retirementYear
|
1965
|
gptkbp:role
|
utility helicopter
|
gptkbp:rotorDiameter
|
36 feet
|
gptkbp:safetyFeatures
|
generally safe for its time
|
gptkbp:services
|
10,000 feet
|
gptkbp:successor
|
Hiller_12
|
gptkbp:type
|
civil helicopter
|
gptkbp:weight
|
2,500 lbs
|
gptkbp:wingspan
|
not applicable
|