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gptkbp:instanceOf
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gptkb:helicopter
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gptkbp:aircraft
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rotorcraft
helicopter configuration
piston engine.
120 knots.
aviation gasoline.
2,200 lbs empty.
2,200 lbs.
3,200 lbs.
not applicable.
10,000 feet.
30 ft 6 in.
300 nautical miles.
9 ft 6 in.
conventional helicopter design.
helicopter.
one of the first successful civilian helicopters.
produced from 1956 to 1965.
utility and training.
coaxial_rotor_system.
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gptkbp:airlines
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1 pilot
1.
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gptkbp:cockpit
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open cockpit
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gptkbp:constructionMaterial
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aluminum
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gptkbp:controls
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cyclic and collective pitch control
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gptkbp:crew
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1
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gptkbp:design
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gptkb:USA
gptkb:Stanley_Hiller_Jr.
two-blade rotor system
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gptkbp:engineConfiguration
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Lycoming.
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gptkbp:enginePower
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200 hp
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gptkbp:engineType
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piston engine
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gptkbp:firstFlight
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1956
1970s
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gptkbp:fuelCapacity
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40 gallons
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gptkbp:headlights
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not applicable
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gptkbp:helicopterCapacity
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3.
40 gallons.
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gptkbp:historicalSignificance
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one of the first successful civilian helicopters.
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https://www.w3.org/2000/01/rdf-schema#label
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Hiller 12C
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gptkbp:introduced
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1956
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gptkbp:landingGear
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skids
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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
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civil aviation
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gptkbp:maxSpeed
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120 knots
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gptkbp:maxTakeoffWeight
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3,200 pounds
3,200 lbs.
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gptkbp:notableFeature
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coaxial_rotor_system
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gptkbp:notableUsers
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gptkb:California_Highway_Patrol
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gptkbp:operationalHistory
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used in various roles including training and utility.
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gptkbp:operationalRange
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300 miles
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gptkbp:passengerCapacity
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3
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gptkbp:primaryUser
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gptkb:United_States_Army
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gptkbp:productionLocation
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gptkb:California,_USA
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gptkbp:productionYears
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1956-1965
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gptkbp:propulsion
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single engine
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gptkbp:range
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300 nautical miles
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gptkbp:relatedAircraft
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gptkb:Hiller_12B
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gptkbp:retired
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1970s
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gptkbp:role
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utility helicopter
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gptkbp:rotorDiameter
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36 feet
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gptkbp:services
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1956
10,000 feet
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gptkbp:successor
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gptkb:Hiller_12E
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gptkbp:totalGoals
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approximately 200
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gptkbp:type
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civil helicopter
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gptkbp:variant
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gptkb:Hiller_12E
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gptkbp:weight
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2,200 pounds
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gptkbp:wingArea
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not applicable
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