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gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:cockpit
|
two-seat cockpit
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:Stanley_Hiller_Jr.
|
|
gptkbp:engineType
|
turbine engine
|
|
gptkbp:firstFlight
|
1964
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|
gptkbp:fuelCapacity
|
100 gallons
|
|
gptkbp:historicalSignificance
|
early civilian helicopter design
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hiller 1100
|
|
gptkbp:influencedBy
|
gptkb:Hiller_360
|
|
gptkbp:introduced
|
1964
|
|
gptkbp:landingGear
|
skids
|
|
gptkbp:length
|
32 feet 6 inches
|
|
gptkbp:manufacturer
|
gptkb:Hiller_Aircraft_Corporation
|
|
gptkbp:marketedAs
|
gptkb:Hiller_1100_Utility_Helicopter
|
|
gptkbp:maxSpeed
|
120 knots
|
|
gptkbp:maxTakeoffWeight
|
4,000 pounds
|
|
gptkbp:notableFeature
|
used in aerial photography
used in news reporting
used in movie filming
used in police operations
used_in_Vietnam_War
coaxial_rotor_system
|
|
gptkbp:operationalArea
|
tourism
law enforcement
medical evacuation
search and rescue
firefighting
|
|
gptkbp:operationalRange
|
250 miles
|
|
gptkbp:passengerCapacity
|
3
|
|
gptkbp:primaryUser
|
gptkb:U.S._military
|
|
gptkbp:productionYears
|
1964-1970
|
|
gptkbp:propulsion
|
single engine
|
|
gptkbp:range
|
300 nautical miles
|
|
gptkbp:relatedModel
|
gptkb:Hiller_12E
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
utility helicopter
|
|
gptkbp:rotorDiameter
|
34 feet
|
|
gptkbp:services
|
10,000 feet
|
|
gptkbp:successor
|
gptkb:Hiller_1200
|
|
gptkbp:totalGoals
|
approximately 100
|
|
gptkbp:type
|
civil helicopter
|
|
gptkbp:variant
|
gptkb:Hiller_1100C
gptkb:Hiller_1100B
|
|
gptkbp:weight
|
2,500 pounds
|