Kaman K-MAX

The Kaman K-MAX (company designation K-1200) is a helicopter with intermeshing rotors (synchropter) designed and produced by the American manufacturer Kaman Aircraft. Developed during the 1980s and 1990s, the K-MAX builds on the work of the German aeronautical engineer Anton Flettner. Performing its maiden flight on December 23, 1991, it was specially designed to optimally perform external cargo load operations and is capable of lifting payloads in excess of 6,000 pounds (2,700 kg), which is greater than the helicopter's empty weight and almost twice as much as the competing Bell 205 despite sharing a similar engine. Being a synchropter, it has greater efficiency in comparison to conventional rotor technology. In addition to airlifting external loads, specialized configurations for aerial firefighting and casualty evacuation have been developed. It was produced for both military and civilian operators. Kaman sought to develop the K-MAX into an unmanned aerial vehicle with optional remote control. During the early 2010s, a pair of unmanned K-Maxes underwent an extended battlefield evaluation as a cargo UAV, for which purpose they were deployed to provide logistics support to United States Marine Corps (USMC) ground forces during the war in Afghanistan. Despite receiving numerous awards, the K-MAX was ultimately passed over by the USMC in favor of an unmanned version of the MD Helicopters MH-6 Little Bird. The company stated its intention to continue development and to seek out other customers for this capability. An optionally piloted configuration, branded as the ’’K-Max Titan’’, underwent flight testing in 2021. The initial production run of the K-MAX ran between 1991 and 2003, at which point the line was shuttered after the completion of 38 helicopters due to low customer demand. During June 2015, Kaman announced that it was restarting production following the receipt of ten commercial orders for the K-MAX. During May 2017, the first flight of a K-MAX built on the
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Kaman Corporation
- Category
- Helicopters
- First flight
- 1991-12-23
Specifications
- Max speed
- 100 kt
- Range
- 300 nm
- Service ceiling
- 15,000 ft
- Rate of climb
- 2,500 ft/min
- Max takeoff weight
- 6,500 lb
- Empty weight
- 5,145 lb
- Fuel capacity
- 228.5 US gal
- Powerplant
- Honeywell T5317A-1
- Engines
- 1
- Seats
- 1
- Length
- 52 ft
- Wingspan
- 51 ft
- Height
- 13 ft
- Number built
- 38
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.