|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:capacity
|
2,722 kg
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crew
|
1
|
|
gptkbp:emptyWeight
|
2,495 kg
|
|
gptkbp:enginePower
|
1,800 shp
|
|
gptkbp:engineType
|
Honeywell T53-17 turboshaft
|
|
gptkbp:FAATypeCertificate
|
1994
|
|
gptkbp:firstFlight
|
1991-12-23
|
|
gptkbp:firstOperator
|
Heli-Air Switzerland
|
|
gptkbp:height
|
4.14 m
|
|
gptkbp:length
|
15.85 m
|
|
gptkbp:mainRotorDiameter
|
14.73 m
|
|
gptkbp:manufacturer
|
gptkb:Kaman_Aerospace
|
|
gptkbp:maximumSpeed
|
185 km/h
|
|
gptkbp:maxTakeoffWeight
|
5,443 kg
|
|
gptkbp:notableFeature
|
intermeshing rotors
unmanned version available
|
|
gptkbp:primaryUser
|
civilian operators
military operators
|
|
gptkbp:range
|
460 km
|
|
gptkbp:role
|
aerial lift helicopter
|
|
gptkbp:serviceCeiling
|
4,880 m
|
|
gptkbp:status
|
in production
|
|
gptkbp:unmannedVariant
|
K-MAX Unmanned Aerial Truck (UAT)
|
|
gptkbp:usedBy
|
gptkb:United_States_Marine_Corps
|
|
gptkbp:usedFor
|
disaster relief
firefighting
logging
cargo resupply
|
|
gptkbp:bfsParent
|
gptkb:Kaman_Corporation
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kaman K-MAX
|