gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:capacity
|
2
|
gptkbp:crew
|
1
|
gptkbp:design
|
single rotor
|
gptkbp:engine
|
Lycoming O-360
|
gptkbp:firstFlight
|
1949
|
gptkbp:firstGeneration
|
gptkb:United_States_Army
|
gptkbp:fuelCapacity
|
200 L
|
gptkbp:headlights
|
not applicable
|
gptkbp:height
|
2.74 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hiller 360
|
gptkbp:influencedBy
|
gptkb:Hiller_1100
Hiller_12
|
gptkbp:landingGear
|
skids
|
gptkbp:length
|
8.23 m
|
gptkbp:manufacturer
|
gptkb:Hiller_Aircraft_Corporation
|
gptkbp:maxSpeed
|
160 km/h
|
gptkbp:maxTakeoffWeight
|
1,600 kg
|
gptkbp:notableFeature
|
high maneuverability
low noise levels
easy maintenance
two-bladed
pioneering design
|
gptkbp:numberBuilt
|
approximately 100
|
gptkbp:productionYears
|
1949-1956
|
gptkbp:range
|
500 km
|
gptkbp:relatedTo
|
gptkb:Hiller_12S
gptkb:Hiller_12X
gptkb:Hiller_12V
gptkb:Hiller_12E
gptkb:Hiller_12R
gptkb:Hiller_12W
gptkb:Hiller_12Y
gptkb:Hiller_12T
Hiller_12Z
Hiller_12A
|
gptkbp:role
|
utility helicopter
|
gptkbp:rotorDiameter
|
10.67 m
|
gptkbp:services
|
3,000 m
|
gptkbp:successor
|
Hiller_12
|
gptkbp:type
|
civil helicopter
|
gptkbp:usedIn
|
civil aviation
|
gptkbp:variant
|
gptkb:Hiller_360B
gptkb:Hiller_360C
Hiller 360A
Hiller 360D
|
gptkbp:weight
|
1,200 kg
|