gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
gptkbp:crew
|
1
|
gptkbp:design
|
single rotor
|
gptkbp:engineType
|
turbine engine
|
gptkbp:firstFlight
|
1960
|
gptkbp:fuelCapacity
|
300 L
|
gptkbp:headlights
|
1
|
gptkbp:height
|
2.74 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hiller 360C-3
|
gptkbp:introduced
|
1960
|
gptkbp:length
|
9.14 m
|
gptkbp:manufacturer
|
gptkb:Hiller_Aircraft_Corporation
|
gptkbp:maxSpeed
|
150 km/h
|
gptkbp:maxTakeoffWeight
|
1,800 kg
|
gptkbp:notableFeature
|
2
low noise operation
high maneuverability
compact design
easy maintenance
|
gptkbp:passengerCapacity
|
2
|
gptkbp:range
|
500 km
|
gptkbp:relatedAircraft
|
gptkb:Hiller_12L
gptkb:Hiller_12G
gptkb:Hiller_12K
gptkb:Hiller_12N
gptkb:Hiller_12H
gptkb:Hiller_12J
gptkb:Hiller_12Q
gptkb:Hiller_12S
gptkb:Hiller_12P
gptkb:Hiller_12C
gptkb:Hiller_12F
gptkb:Hiller_12M
gptkb:Hiller_12X
gptkb:Hiller_12V
gptkb:Hiller_12E
gptkb:Hiller_12R
gptkb:Hiller_12W
gptkb:Hiller_12B
gptkb:Hiller_12D
gptkb:Hiller_12Y
gptkb:Hiller_12T
Hiller_12I
Hiller_12O
Hiller_12U
Hiller_12Z
|
gptkbp:retired
|
1970
|
gptkbp:role
|
utility helicopter
|
gptkbp:rotorDiameter
|
10.67 m
|
gptkbp:services
|
3,000 m
|
gptkbp:successor
|
Hiller_12
|
gptkbp:usedBy
|
military
civilian
|
gptkbp:variant
|
Hiller_360C-3A
Hiller_360C-3B
|
gptkbp:weight
|
1,200 kg
|