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gptkbp:instanceOf
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gptkb:helicopter
|
|
gptkbp:aircraft
|
civilian_helicopter
|
|
gptkbp:capacity
|
2 passengers
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|
gptkbp:cockpit
|
open cockpit
|
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gptkbp:crew
|
1
|
|
gptkbp:design
|
single rotor
Henry_Hiller
|
|
gptkbp:developer
|
Hiller_12_series
|
|
gptkbp:electrification
|
Lycoming VO-540
|
|
gptkbp:enginePower
|
260 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1956
|
|
gptkbp:fuelCapacity
|
40 gallons
|
|
gptkbp:headlights
|
two-blade
|
|
gptkbp:historicalSignificance
|
first helicopter with a fenestron tail rotor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hiller 12M
|
|
gptkbp:influencedBy
|
Hiller_12A
|
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gptkbp:introduced
|
1956
|
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gptkbp:landingGear
|
skids
|
|
gptkbp:legacy
|
influenced modern helicopter design.
|
|
gptkbp:length
|
30 feet 6 inches
|
|
gptkbp:manufacturer
|
gptkb:Hiller_Aircraft_Company
|
|
gptkbp:maxSpeed
|
120 knots
|
|
gptkbp:maxTakeoffWeight
|
3,000 pounds
|
|
gptkbp:notableFeature
|
fenestron tail rotor
|
|
gptkbp:operationalArea
|
search and rescue
|
|
gptkbp:operationalRange
|
200 miles
|
|
gptkbp:primaryUser
|
United_States_Army,_United_States_Navy
|
|
gptkbp:produces
|
1956-1970
|
|
gptkbp:propulsion
|
turbine engine
|
|
gptkbp:range
|
300 miles
|
|
gptkbp:relatedAircraft
|
gptkb:Bell_47
|
|
gptkbp:relatedModel
|
gptkb:Hiller_12B
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:retirementYear
|
outdated technology
|
|
gptkbp:role
|
utility
|
|
gptkbp:rotorDiameter
|
36 feet
|
|
gptkbp:serviceHistory
|
used in various military operations
|
|
gptkbp:services
|
10,000 feet
|
|
gptkbp:successor
|
gptkb:Hiller_12E
|
|
gptkbp:totalGoals
|
over 1,000
|
|
gptkbp:type
|
light utility helicopter
|
|
gptkbp:usedBy
|
gptkb:United_States_Army
|
|
gptkbp:variant
|
gptkb:Hiller_12E
|
|
gptkbp:weight
|
1,800 pounds
|