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Kaman K-1200 / K-MAX

kamankmax

First flew on 23 December 1991. Certification and initial deliveries took place in 1994. Using intermeshing main rotors, no tail rotor is required.

Kaman K-Max
Engine: Textron Lycoming T 5317 A1, 1479 shp
Instant pwr: 1118 kW.
Length: 51.837 ft / 15.8 m
Height: 13.583 ft / 4.14 m
Rotor diameter: 48.228 ft / 14.7 m
Max take off weight: 11501.3 lb / 5216.0 kg
Weight empty: 4701.1 lb / 2132.0 kg
Payload: 2722 kg
Max. speed: 100 kts / 185 kph
Max cruise: 100 kts
Service ceiling: 25000 ft / 7620 m
Crew: 1
Payload: max 2700kg ext.
 


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